Calculator A to Z

Calculators Created by Maiarutselvan V

Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
https://www.linkedin.com/in/maiarutselvan-v-ba5533149/
301
Formulas Created
274
Formulas Verified
115
Across Categories

List of Calculators by Maiarutselvan V

Following is a combined list of all the calculators that have been created and verified by Maiarutselvan V. Maiarutselvan V has created 301 and verified 274 calculators across 115 different categories till date.
Absolute Temperature (2)
Created Absolute Temperature for Velocity of Sound Wave in Isothermal Process
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Created Absolute Temperature for Velocity of Sound Wave using Adiabatic Process
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Aerodynamic Nomenclature (5)
Verified Normal force coefficient with aerodynamic normal force
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Verified Rolling moment
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Verified Rolling moment coefficient
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Verified Velocity along pitch axis for small sideslip angle
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Verified Velocity along roll axis for small angle of attack
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12 More Aerodynamic Nomenclature Calculators
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Airfoil (5)
Created Angle of Attack for Circulation developed on Airfoil
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Created Angle of Attack for Lift Coefficient on Airfoil
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Created Chord Length for Circulation developed on Airfoil
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Created Circulation developed on Airfoil
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Created Coefficient of Lift for Airfoil
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Altitude Effects on Power Required and Available (2)
Verified Power required at Altitude
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Verified Power required at Altitude given Power at sea-level
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5 More Altitude Effects on Power Required and Available Calculators
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Approximate Results Applied to Hypersonic Vehicles (5)
Verified Coefficient of drag over flat under freestream flow conditions
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Verified Drag force over flat plate
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Verified Freestream Stanton number for flat plate
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Verified Local heat transfer over flat plate using Stanton number
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Verified Pressure ratio for insulated flat plate, weak interaction
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10 More Approximate Results Applied to Hypersonic Vehicles Calculators
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Basic Compressible Flow (1)
Verified Ratio of stagnation and static pressure
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5 More Basic Compressible Flow Calculators
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Basic Formulas (9)
Created Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle
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Created Area of Pipe for Maximum Power Transmission through Nozzle
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Created Coefficient of contraction for sudden contraction
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Created Difference in liquid level in three compound pipes with same friction coefficient
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Created Discharge in Equivalent Pipe
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Created Maximum Area of Obstruction in Pipe
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Created Power Lost ue to Sudden Enlargement
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Created Power transmission through pipes
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Created Time taken by pressure wave to travel
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3 More Basic Formulas Calculators
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Basics (3)
Verified Friction Coefficient
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Verified Mach Number
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Verified Stagnation Temperature
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5 More Basics Calculators
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Blast-wave part 2 (1)
Verified Pressure coefficient for blast wave theory
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5 More Blast-wave part 2 Calculators
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Bodies connected by string and lying on rough inclined planes (5)
Verified Acceleration of system for given mass of body A
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Verified Acceleration of system for given mass of body B
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Verified Frictional force on body B
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Verified Tension in string for given mass of body A
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Verified Tension in string for given mass of body B
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1 More Bodies connected by string and lying on rough inclined planes Calculators
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Bodies connected by string and lying on smooth inclined planes (2)
Verified Angle of inclination of plane with body A
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Verified Angle of inclination of plane with body B
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2 More Bodies connected by string and lying on smooth inclined planes Calculators
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Bodies connected by string, one hanging free, other lying on a rough inclined plane (2)
Verified Coefficient of friction for given frictional force
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Verified Frictional force
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5 More Bodies connected by string, one hanging free, other lying on a rough inclined plane Calculators
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Bodies connected by string, one hanging free, other lying on smooth inclined plane (1)
Verified Tension in string when one body is lying on smooth inclined plane
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3 More Bodies connected by string, one hanging free, other lying on smooth inclined plane Calculators
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Boundary Layer Flow (21)
Created Area of surface for average drag coefficient in boundary layer flows
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Created Average coefficient of drag for drag force in boundary layer flows
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Created Coefficient of drag for Blasius's solution in boundary layer flow
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Created Coefficient of Drag for Reynold number in Laminar Boundary Layer Flow
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Created Distance from leading edge for Blasius's solution in boundary layer flow
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Created Distance from leading edge in boundary layer flow
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Created Drag force for average drag coefficient in boundary layer flows
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Created Drag Force on Plate in Boundary Layer Flow
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Created Freestream velocity for local drag coefficient in boundary layer flows
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Created Length of Plate for Reynold number in Laminar Boundary Layer Flow
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Created Local drag coefficient for shear stress in boundary layer flows
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Created Reynold number at end of plate
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Created Reynold number for drag coefficient in Blasius's solution of boundary layer flow
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Created Reynold number for Drag Force on Plate in Boundary Layer Flow
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Created Shear Stress at Boundary for Turbulent Boundary Layer over Flat Plate
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Created Shear stress for local drag coefficient in boundary layer flows
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Created Thickness of boundary layer for Blasius's solution in boundary layer flow
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Created Thickness of boundary layer in boundary layer flow
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Created Velocity of fluid for Reynold number in Laminar Boundary Layer Flow
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Created Viscosity of Liquid for Drag Force on Plate in Boundary Layer Flow
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Created Width of Plate for Drag Force on Plate in Boundary Layer Flow
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Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions (13)
Verified Dynamic viscosity around wall
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Verified Local heat transfer rate using Nusselt's number
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Verified Local heat-transfer rate calculation using Stanton number
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Verified Local shear stress at wall
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Verified Nusselt's number with Reynolds number, Stanton number and Prandtl number
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Verified Prandtl number with Reynolds number, Nusselt's number, and Stanton number
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Verified Stanton number for hypersonic vehicle
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Verified Static Density equation using skin friction coefficient
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Verified Static density equation using Stanton number
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Verified Static velocity equation using skin friction coefficient
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Verified Static velocity using Stanton number
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Verified Static viscosity relation using temperature of wall
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Verified Thermal conductivity at edge of boundary layer equation using Nusselt's number
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7 More Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions Calculators
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Buoyancy (9)
Created Angle of heel for metacentric height in experimental method
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Created Centre of Buoyancy
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Created Meta-centric height for time period of oscillation and radius of gyration
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Created Meta-centric height in experimental method
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Created Movable weight for metacentric height in experimental method
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Created Radius of gyration for metacentric height and time period of oscillation
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Created Time Period of Oscillation of Ship
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Created Volume of body in fluid for metacentric height and BG
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Created Volume of fluid displaced
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2 More Buoyancy Calculators
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Circulation (3)
Created Circulation for Lift Force on Cylinder
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Created Circulation for Single Stagnation Point
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Created Circulation in Location of Stagnation Points
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1 More Circulation Calculators
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Coefficient of Discharge (5)
Created Coefficient of discharge
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Created Coefficient of discharge for area and velocity
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Created Coefficient of Discharge given Time for Emptying Tank
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Created Coefficient of Discharge given Time of Emptying Circular Horizontal Tank
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Created Coefficient of Discharge given Time of Emptying Hemispherical Tank
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Coefficient of Velocity (3)
Created Coefficient of velocity
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Created Coefficient of velocity for horizontal and vertical distance
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Created Coefficient of Velocity given Head Loss
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Coefficient's (5)
Created Coefficient of drag for sphere in Oseen formula when Reynolds number is between 0.2 and 5
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Created Coefficient of drag for sphere in stoke's law when Reynolds number is less than 0.2
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Created Lift coefficient for lift force in body moving on fluid
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Created Lift Coefficient for Rotating Cylinder with Circulation
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Created Lift Coefficient for Rotating Cylinder with Tangential Speed
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Compressible Flow (7)
Created Bulk Modulus for Velocity of Sound Wave
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Created Mach angle for Compressible Fluid Flow
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Created Mach number for Compressible Fluid Flow
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Created Pressure ratio for maximum flow rate through nozzle or orifice
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Created Temperature of fluid for stagnation temperature considering compressible fluid flow
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Created Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid
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Created Velocity of projectile of mach cone in compressible fluid flow
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COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS (2)
Verified Emissivity
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Verified Reference viscosity
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2 More COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS Calculators
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Contribution of Aircraft Components- Part 1 (1)
Verified Sideslip angle for Aircraft
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14 More Contribution of Aircraft Components- Part 1 Calculators
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Contribution of Aircraft Components- Part 2 (3)
Verified Wing area for given moment produced by vertical tail
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Verified Wing dynamic pressure for given yawing moment coefficient
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Verified Wingspan for given yawing moment coefficient
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11 More Contribution of Aircraft Components- Part 2 Calculators
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Cutting Force (2)
Created Cutting Force for Frictional Force along Tool Rake Face and Thrust Force
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Created Cutting Force given Shear Force and Thrust Force
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4 More Cutting Force Calculators
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Cylinders (2)
Verified Convection Resistance for Cylindrical Layer
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Verified Length of cylindrical wall for given heat flow rate
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12 More Cylinders Calculators
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Diameter and Length of Pipe (4)
Created Diameter of Equivalent Pipe
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Created Diameter of nozzle for maximum power transmission through nozzle
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Created Length of Equivalent Pipe
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Created Length of pipe for maximum power transmission through nozzle
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Diameter of Pipe (3)
Created Diameter of pipe for difference in pressure in viscous flow
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Created Diameter of pipe for head loss due to friction in viscous flow
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Created Diameter of pipe for loss of pressure head in viscous flow
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Discharge (6)
Created Discharge in Borda's Mouthpiece Running Free
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Created Discharge in Borda's Mouthpiece Running Full
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Created Discharge in Convergent-Divergent Mouthpiece
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Created Discharge through fully sub-merged orifice
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Created Discharge through large rectangular orifice
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Created Discharge through partially sub-merged orifice
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Discharge (13)
Created Coefficient of Discharge for Time required to Empty Reservoir
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Created Discharge over Broad-crested Weir
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Created Discharge over Broad-Crested Weir for Head of Liquid at Middle
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Created Discharge over broad-crested weir with velocity approach
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Created Discharge over rectangle notch or weir
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Created Discharge over rectangle weir considering Bazin's formula
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Created Discharge over rectangle weir considering Francis's formula
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Created Discharge over rectangle weir for Bazin's formula with velocity approach
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Created Discharge over rectangle weir with two end contractions
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Created Discharge over Trapezoidal Notch or Weir
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Created Discharge over Triangular Notch or Weir
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Created Discharge with velocity of approach
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Created Discharge without velocity of approach
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Drag during Level Unaccelerated Flight (2)
Verified Zero-lift drag coefficient at minimum required thrust
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Verified Zero-lift drag coefficient for given required thrust
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5 More Drag during Level Unaccelerated Flight Calculators
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Drag Force on Body (4)
Created Drag Force for body moving in Fluid of Certain Density
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Created Pressure Drag from Total Drag Force on Sphere
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Created Skin Friction Drag from Total Drag Force on Sphere
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Created Total Drag force on Sphere
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3 More Drag Force on Body Calculators
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Dynamics of Fluid Flow (6)
Created Actual discharge in venturimeter
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Created Coefficient of pitot-tube for velocity at any point
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Created Difference in pressure head for heavier liquid in manometer
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Created Difference in pressure head for light liquid in manometer
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Created Resultant bend force along x and y direction
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Created Velocity at any point for coefficient of pitot-tube
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1 More Dynamics of Fluid Flow Calculators
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ELEMENTS OF KINETIC THEORY (10)
Verified Emissivity per unit mole
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Verified Kinetic energy per mole
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Verified Kinetic energy per mole using molar volume
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Verified Kinetic energy per mole using temperature of gas
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Verified Mean free path of single-species gas
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Verified Pressure using kinetic energy per mole
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Verified Pressure using molar volume
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Verified Specific gas constant using kinetic energy per mole
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Verified Temperature of gas using Emissivity per unit mole
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Verified Temperature of gas using kinetic energy per mole
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5 More ELEMENTS OF KINETIC THEORY Calculators
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Elevator and Stick Deflection Angles (1)
Verified Stick deflection angle for given stick force
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3 More Elevator and Stick Deflection Angles Calculators
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Enthalpy and Velocity (2)
Verified Static enthalpy behind normal shock for given upstream enthalpy and Mach number
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Verified Static enthalpy ratio across normal shock
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9 More Enthalpy and Velocity Calculators
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Flat-Plate for Viscous flow case (8)
Verified Aerodynamic Heating Equation for Stanton number
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Verified Coefficient of friction using Stanton number for flat plat case
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Verified Drag per unit span
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Verified Prandtl number for flat plate with viscous flow
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Verified Recovery Factor using temperature
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Verified Skin-friction drag for flat plate in viscous flow
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Verified Static density equation using aerodynamic equation
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Verified Static velocity equation using aerodynamic heating equation
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7 More Flat-Plate for Viscous flow case Calculators
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Flight Envelope (4)
Verified Load factor for given turn radius for high-performance fighter aircraft
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Verified Turn radius for high load factor
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Verified Turn rate for given lift coefficient
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Verified Velocity given Turn Radius for High Load Factor
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12 More Flight Envelope Calculators
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Flow in Open Channels (19)
Created Area of Flow for Circular Channel
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Created Bazin's constant
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Created Chezy's constant considering Bazin formula
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Created Chezy's constant considering Kutter's formula
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Created Chezy's constant considering Manning's formula
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Created Chezy's constant considering velocity
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Created Critical depth considering flow in open channels
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Created Critical depth considering minimum specific energy
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Created Critical Depth using Critical Velocity
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Created Critical velocity considering flow in open channels
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Created Discharge per unit width considering flow in open channels
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Created Hydraulic mean depth considering Bazin formula
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Created Hydraulic mean depth considering Manning's formula
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Created Hydraulic mean depth using Chezy's formula
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Created Manning's coefficient or constant
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Created Minimum Specific Energy using Critical Depth
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Created Radius of Circular Channel using Wetted Perimeter
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Created Velocity of Chezy's formula
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Created Wetted Perimeter for Circular Channel
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Force Along The Shear (2)
Created Force along shear force for given force normal to shear force, shear, friction and normal rake angle
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Created Force along Shear Force given Cutting Force and Thrust Force
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1 More Force Along The Shear Calculators
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Force Normal To Shear (1)
Created Force normal to shear force for given cutting force, thrust force, and shear angle
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1 More Force Normal To Shear Calculators
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Fundamentals of Inviscid Incompressible flow (6)
Verified 2-D Lift coefficient for cylinder
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Verified Airspeed measurement by venturi
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Verified Freestream density by Kutta-Joukowski theorem
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Verified Freestream velocity by Kutta-Joukowski theorem
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Verified Test section velocity for low speed wind tunnel given height difference of manometric fluid
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Verified Test section velocity in low-speed wind tunnel
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9 More Fundamentals of Inviscid Incompressible flow Calculators
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Gain (1)
Verified Current Gain of Amplifier in Decibels
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15 More Gain Calculators
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Gearing Ratio (2)
Verified Gearing ratio
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Verified Gearing ratio for given hinge moment coefficient
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2 More Gearing Ratio Calculators
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Geometry of Turning Process (4)
Created Feed force
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Created Radial force
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Created Side cutting edge angle for orthogonal cutting
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Created Side rake angle for orthogonal cutting
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6 More Geometry of Turning Process Calculators
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Gliding Flight (1)
Verified Glide angle for given lift-to-drag ratio
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4 More Gliding Flight Calculators
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Head Available (3)
Created Head available at Base of Nozzle
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Created Total head at inlet of pipe for head available at base of nozzle
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Created Total head available at inlet of pipe for efficiency of power transmission
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Hinge Moment (2)
Verified Hinge moment for given gearing ratio
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Verified Hinge moment for given stick force
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1 More Hinge Moment Calculators
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Hypersonic Equivalence Principle and Blast-Wave Theory (4)
Verified Energy for blast wave
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Verified Radial coordinate of blunt slab blast wave
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Verified Simplified pressure ratio for blunt cylinder blast wave
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Verified Time required for blast wave
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12 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
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Hypersonic Flight Paths: Velocity-Altitude Map (4)
Verified Pressure ratio of Blunt-nosed cylinder (first approximation)
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Verified Radial coordinate of Blunt-nosed cylinder (first approximation)
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Verified Radius for cylinder-wedge body shape
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Verified Radius for sphere-cone body shape
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5 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators
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Hypersonic Flow (3)
Verified Mach ratio at high mach number
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Verified Pressure ratio for high Mach number
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Verified Pressure ratio having high mach number with similarity constant
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17 More Hypersonic Flow Calculators
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Hypersonic Inviscid Flowfields: Approximate Methods (3)
Verified Non-dimensional pressure
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Verified Non-dimensional pressure for high mach number
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Verified Slenderness ratio with cone radius for hypersonic vehicle
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8 More Hypersonic Inviscid Flowfields: Approximate Methods Calculators
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Hypersonic Inviscid Flowfields: Exact Methods (7)
Verified Detachment distance of cylinder wedge body shape
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Verified Detachment distance of sphere cone body shape
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Verified Grid point calculation for shock waves
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Verified Nose radius of cylinder-wedge
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Verified Nose radius of sphere cone
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Verified Pressure ratio for unsteady waves
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Verified Ratio of new and old temperature
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11 More Hypersonic Inviscid Flowfields: Exact Methods Calculators
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Hypersonic Small-Disturbance Equations (6)
Verified Change in velocity for hypersonic flow in x direction
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Verified Coefficient of pressure with slenderness ratio and similarity constant
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Verified Constant g used for finding location of perturbed shock
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Verified Density ratio with similarity constant having slenderness ratio
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Verified Distance from tip of leading edge to base
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Verified Non- dimensionalised time
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11 More Hypersonic Small-Disturbance Equations Calculators
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Hypersonic Transition (13)
Verified Boundary-layer momentum thickness using Reynolds number at transition point
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Verified Eddy viscosity calculation
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Verified Local Mach Number using Reynolds number equation at transition region
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Verified Location of transition point
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Verified Prandtl number of transition flow
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Verified Specific heat at constant pressure for transient flow
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Verified Static density at transition point
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Verified Static density equation using boundary-layer momentum thickness
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Verified Static velocity at transition point
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Verified Static velocity using boundary-layer momentum thickness
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Verified Static viscosity at transition point
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Verified Static viscosity equation using boundary-layer momentum thickness
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Verified Transition Reynolds number
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3 More Hypersonic Transition Calculators
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Hypersonic Viscous Interactions (9)
Verified Large Mach number over flat plate using static temperature and wall temperature
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Verified Pressure Ratio for Cold-Wall case Strong Interaction
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Verified Pressure Ratio for Cold-Wall case Weak Interaction
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Verified Static density of fluid over flat plate
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Verified Static temperature over flat plate using Static Mach Number
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Verified Static viscosity using wall temperature and static temperature
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Verified viscosity of wall using wall temperature and static temperature
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Verified Wall density of fluid over flat plate
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Verified Wall temperature over flat plate using Static Mach Number
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9 More Hypersonic Viscous Interactions Calculators
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Ideal flow or Potential flow (14)
Created Dimensions of Rankine half-body
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Created Distance of stagnation point S from source in flow past half body
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Created Location of stagnation point on x-axis
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Created Radial velocity at any radius
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Created Radius at any point considering radial velocity
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Created Radius of Rankine circle
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Created Stream function at point
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Created Stream Function at Point in Combined Flow
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Created Stream function in sink flow for angle
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Created Strength of doublet for stream function
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Created Strength of source for radial velocity and at any radius
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Created Strength of source for Rankine half body
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Created Uniform flow velocity for Rankine half body
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Created Uniform flow velocity for stream function at point in combined flow
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Incompressible flow over airfoil (2)
Verified Boundary layer thickness for laminar flow
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Verified Moment coefficient about leading-edge for symmetrical airfoil by thin airfoil theory
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6 More Incompressible flow over airfoil Calculators
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Kinematics of flow (7)
Created Angular Velocity of Vortex using Depth of Parabola
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Created Depth of Parabola formed at Free Surface of Water
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Created Height or depth of paraboloid for volume of air
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Created Rate of flow or discharge
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Created Resultant velocity for two velocity components
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Created Total Pressure Force at Bottom of Cylinder
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Created Total pressure force on top of cylinder
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Laminar boundary layer at a stagnation point on a blunt body, (5)
Verified Newtonian Dynamic pressure
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Verified Newtonian Pressure distribution over Surface using Cosine Angle
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Verified Nusselt number at stagnation point
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Verified Nusselt number for stagnation point on blunt body
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Verified Stagnation pressure
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2 More Laminar boundary layer at a stagnation point on a blunt body, Calculators
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Landing Performance (1)
Verified Touchdown velocity
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3 More Landing Performance Calculators
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Length of Pipe (3)
Created Length of pipe for difference of pressure in viscous flow
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Created Length of pipe for head loss due to friction in viscous flow
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Created Length of pipe for loss of pressure head in viscous flow
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Length of Weir (8)
Created Length of weir considering Bazin's formula with velocity approach
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Created Length of weir considering Bazin's formula without velocity approach
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Created Length of weir considering Francis's formula
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Created Length of weir for broad-crested weir and head of liquid at middle
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Created Length of weir for broad-crested weir with velocity approach
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Created Length of Weir for Discharge over Broad-Crested Weir
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Created Length of weir or notch for velocity of approach
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Created Length of weir or notch without velocity of approach
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Lift Force on Body (4)
Created Area of body for Lift Force in body moving on Fluid
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Created Length of Cylinder for Lift Force on Cylinder
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Created Lift Force for body moving in Fluid of Certain Density
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Created Lift Force on Cylinder for Circulation
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3 More Lift Force on Body Calculators
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Lift to Drag (3)
Verified Lift-to-drag ratio for given required thrust of aircraft
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Verified Thrust of aircraft required for given Lift-to-drag ratio
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Verified Weight of aircraft for given Lift-to-drag ratio
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Longitudinal Control of Elevator Hinge Moment (3)
Verified Elevator area for given hinge moment coefficient
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Verified Elevator Hinge moment coefficient
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Verified Elevator Hinge moment for given hinge moment coefficient
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2 More Longitudinal Control of Elevator Hinge Moment Calculators
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Loss of Head (8)
Created Head Loss due to Friction for Efficiency of Power Transmission
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Created Loss of head at entrance of pipe
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Created Loss of head at exit of pipe
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Created Loss of head due to bead in pipe
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Created Loss of head due to obstruction in pipe
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Created Loss of head due to sudden contraction
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Created Loss of head due to sudden enlargement at any particular section of pipe
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Created Loss of head in equivalent pipe
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Loss of Head (3)
Created Loss of head due to friction
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Created Loss of pressure head for viscous flow between two parallel plates
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Created Loss of pressure head for viscous flow through circular pipe
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Maneuvering Flight (7)
Verified Load Factor given Pull-down Maneuver Radius
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Verified Load Factor given Pull-Up Maneuver Rate
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Verified Pull-down maneuver radius
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Verified Pull-up maneuver rate
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Verified Velocity for given pull-down maneuver rate
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Verified Velocity for given pull-up maneuver radius
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Verified Velocity for given pull-up maneuver rate
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6 More Maneuvering Flight Calculators
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Merchant Force Circle (Mechanics of Orthogonal metal cutting) (1)
Created Frictional force along tool rake face for given cutting and thrust forces, normal rake angle
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21 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
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Newtonian Flow (5)
Verified Coefficient of drag equation with coefficient of normal force
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Verified Exact normal shock wave maximum coefficient of pressure
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Verified Force Exerted on Surface given Static Pressure
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Verified Mass Flux Incident on Surface Area
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Verified Maximum Pressure coefficient
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9 More Newtonian Flow Calculators
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Normal Shock Waves (4)
Verified Density behind normal shock for given upstream density and Mach number
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Verified Static pressure behind normal shock for given upstream pressure and Mach number
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Verified Static temperature behind normal shock for given upstream temperature and Mach number
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Verified Temperature Ratio across Normal Shock
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16 More Normal Shock Waves Calculators
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Notches and Weirs (6)
Created Head of Liquid above V-notch
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Created Head of Liquid at Crest
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Created Length of Crest of Weir or Notch
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Created Length of section for discharge over rectangle notch or weir
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Created Time required to Empty Reservoir
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Created Time required to empty tank with Triangular Weir or Notch
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Oblique Shock and Expansion Waves (10)
Verified Component of downstream Mach number normal to oblique shock for given normal upstream Mach number
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Verified Density behind oblique shock for given upstream density and normal upstream Mach number
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Verified Density Ratio across Oblique Shock
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Verified Forward Mach angle of expansion fan
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Verified Pressure behind oblique shock for given upstream pressure and normal upstream Mach number
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Verified Pressure Ratio across Expansion Fan
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Verified Pressure Ratio across Oblique shock
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Verified Temperature behind oblique shock for given upstream temperature and normal upstream Mach number
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Verified Temperature Ratio across Expansion Fan
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Verified Temperature Ratio across Oblique Shock
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9 More Oblique Shock and Expansion Waves Calculators
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oblique shock relation (2)
Verified Parallel upstream flow components after shock as Mach tends to infinite
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Verified Perpendicular Upstream Flow Components behind Shock Wave
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13 More oblique shock relation Calculators
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Orifices and Mouthpieces (16)
Created Absolute pressure head at constant head and atmospheric pressure head
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Created Area at vena contracta for discharge and constant head
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Created Area of Mouthpiece in Borda's Mouthpiece Running Free
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Created Area of Mouthpiece in Borda's Mouthpiece Running Full
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Created Area of Orifice given Time of Emptying Hemispherical Tank
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Created Area of Tank given Time for Emptying Tank
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Created Atmospheric pressure head at constant head and absolute pressure head
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Created Coefficient of Contraction given Area of Orifice
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Created Head of Liquid above Centre of Orifice
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Created Head of liquid for head loss and coefficient of velocity
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Created Horizontal distance for coefficient of velocity and vertical distance
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Created Loss of head due to fluid resistance
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Created Loss of head due to sudden enlargement
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Created Theoretical velocity
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Created Velocity of liquid at C-C for Hc, Ha, and H
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Created Vertical distance for coefficient of velocity and horizontal distance
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Plane walls (10)
Verified Area of composite wall of 2 layers
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Verified Area of composite wall of 3 layers
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Verified Inner Surface Temperature of Composite Wall for 2 Layers in Series
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Verified Inner Surface Temperature of Composite Wall of 3 Layers in Series
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Verified Inner Surface Temperature of Plane Wall
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Verified Length of 3rd Layer of Composite Wall in Conduction through Walls
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Verified Temperature at distance x from Inner Surface in Wall
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Verified Thermal Resistance of Composite Wall with 2 layers in Series
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Verified Thermal Resistance of Composite Wall with 3 Layers in Series
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Verified Thermal Resistance of Wall
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12 More Plane walls Calculators
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Power Absorbed (3)
Created Power absorbed in collar bearing
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Created Power absorbed in foot-step bearing
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Created Power absorbed in overcoming viscous resistance in journal bearing
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Power Available and Maximum Velocity (2)
Verified Power available for reciprocating engine-propeller combination
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Verified Propeller efficiency for reciprocating engine-propeller combination
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1 More Power Available and Maximum Velocity Calculators
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Power Required for Level Unaccelerated Flight (2)
Verified Power required for given total drag force
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Verified Total drag force for given required power
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8 More Power Required for Level Unaccelerated Flight Calculators
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Power Transmission Efficiency (3)
Created Efficiency of power transmission in flow through pipes
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Created Efficiency of Power Transmission through Nozzle
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Created Efficiency of power transmission through nozzle for velocity and total head
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Pressure (3)
Verified Dynamic pressure in incompressible flow
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Verified Pressure difference measured by manometer in low-speed wind tunnel
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Verified Total pressure in incompressible flow
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10 More Pressure Calculators
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Pressure and Density (4)
Created Density of fluid considering velocity at outlet of orifice
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Created Density of Fluid for Stagnation considering Compressible Fluid Flow
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Created Pressure at inlet considering maximum flow rate of fluid
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Created Pressure at Inlet of Tank or Vessel considering Compressible Fluid Flow
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Radial Velocity (1)
Verified Radial velocity for 2-D incompressible source flow
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2 More Radial Velocity Calculators
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Range and Endurance of Propeller-Driven Airplane (9)
Verified Endurance of Propeller-Driven Airplane
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Verified Propeller Efficiency for given Endurance of Propeller-Driven Airplane
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Verified Propeller Efficiency for given Range and lift-to-drag ratio of Propeller-Driven Airplane
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Verified Propeller Efficiency for given Range of Propeller-Driven Airplane
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Verified Range of Propeller-Driven Airplane
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Verified Range of Propeller-Driven Airplane for given lift-to-drag ratio
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Verified Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
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Verified Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane
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Verified Specific Fuel Consumption for given Range of Propeller-Driven Airplane
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1 More Range and Endurance of Propeller-Driven Airplane Calculators
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Rate of Climb (1)
Verified Thrust available for given excess power
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9 More Rate of Climb Calculators
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Reference Temperature Method (8)
Verified Chord length for flat plate case
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Verified Local Reynolds number
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Verified Mach number at reference temperature
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Verified Overall skin-friction drag coefficient for incompressible flow
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Verified Reference temperature equation
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Verified Stanton Number obtained from classical theory
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Verified Static viscosity of plate using chord length for flat plate case
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Verified Wall temperature using reference temperature
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7 More Reference Temperature Method Calculators
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Roll Stability (5)
Verified Aircraft forward velocity for given normal component of side velocity
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Verified Aircraft sideslip velocity for given dihedral angle
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Verified Dihedral angle for given sideslip velocity
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Verified Normal component of aircraft side velocity for given dihedral angle
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Verified Normal component of aircraft side velocity for given forward velocity
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Rotational Speed (3)
Created Rotational speed considering power absorbed and torque in journal bearing
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Created Rotational speed for torque required in collar bearing
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Created Rotational speed for torque required in foot-step bearing
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Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations (5)
Verified Coefficient of pressure equation using specific heat ratio
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Verified curvilinear grid location equation
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Verified Density equation using enthalpy and pressure
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Verified Enthalpy equation using pressure and density
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Verified pressure equation using Enthalpy and density
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6 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators
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Spheres (9)
Verified Convection Resistance for Spherical Layer
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Verified Heat flow rate through spherical composite wall of 2 layers in series
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Verified Inner Surface Temperature of Spherical Wall
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Verified Outer Surface Temperature of Spherical Wall
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Verified Thermal Resistance of Spherical Composite Wall of 2 layers in Series with Convection
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Verified Thickness of Spherical Wall to Maintain given Temperature Difference
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Verified Total Thermal Resistance of Spherical Wall of 2 Layers without Convection
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Verified Total Thermal Resistance of Spherical wall of 3 Layers without Convection
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Verified Total Thermal Resistance of Spherical Wall with Convection on both side
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2 More Spheres Calculators
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Stagnation Density (2)
Created Stagnation Density considering other Stagnation properties of Fluid
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Created Stagnation Density given Compressible Fluid Flow
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Stagnation Points (4)
Created Location of Stagnation points for Rotating Cylinder in Uniform Flow Field
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Created Radius of Cylinder for Lift Coefficient in Rotating Cylinder with Circulation
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Created Radius of Cylinder for location of Stagnation Points
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Created Radius of Cylinder for Single Stagnation Point
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Stagnation Pressure (2)
Created Stagnation Pressure considering other Stagnation Properties of Fluid
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Created Stagnation Pressure for Compressible Fluid Flow
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Stagnation Temperature (2)
Created Stagnation Temperature considering Compressible Fluid Flow
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Created Stagnation Temperature considering other Stagnation properties of Fluid
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Stick Forces (3)
Verified Elevator area for given stick force
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Verified Flight velocity for given stick force
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Verified Stick length for given stick force
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4 More Stick Forces Calculators
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Stream Function (5)
Verified Stream function for 2-D Doublet flow
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Verified Stream function for 2-D Vortex flow
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Verified Stream Function for Lifting Flow over Circular Cylinder
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Verified Stream function for semi-infinite body
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Verified Stream function for uniform incompressible flow
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4 More Stream Function Calculators
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Tail Contribution (12)
Verified Angle of incidence of tail
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Verified Lift due to tail only
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Verified Lift due to wing only
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Verified Tail area for given tail efficiency
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Verified Tail Efficiency for given lift coefficients
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Verified Tail lift coefficient for given pitching moment
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Verified Tail Lift Coefficient of wing-tail combination
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Verified Tail lift for given tail pitching moment
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Verified Tail Pitching moment coefficient
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Verified Tail Pitching moment for given lift coefficient
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Verified Total Lift of wing-tail combination
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Verified Wing Lift Coefficient of wing-tail combination
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9 More Tail Contribution Calculators
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Tail Contribution Contd (5)
Verified Tail area for given tail moment coefficient
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Verified Tail Efficiency for given pitching moment coefficient
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Verified Tail lift coefficient for given pitching moment coefficient
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Verified Tail moment arm for given tail moment coefficient
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Verified Tail Pitching moment coefficient for given tail efficiency
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9 More Tail Contribution Contd Calculators
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Takeoff Performance (1)
Verified Liftoff velocity for given weight
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13 More Takeoff Performance Calculators
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Tangential Velocity (1)
Verified Tangential velocity for non-lifting flow over circular cylinder
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2 More Tangential Velocity Calculators
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Thickness of Oil Film (3)
Created Thickness of oil film for shear force in journal bearing
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Created Thickness of oil film for speed and diameter of shaft in journal bearing
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Created Thickness of oil film for torque required in foot-step bearing
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Thrust Force (2)
Created Thrust force for given cutting force, shear angle and force along shear force
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Created Thrust force for given cutting force, shear angle and force normal to shear force
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2 More Thrust Force Calculators
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Thrust Required for Level Unaccelerated Flight (5)
Verified Coefficient of Lift for given thrust and weight
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Verified Lift coefficient for given minimum required thrust
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Verified Minimum Thrust required for given lift coefficient
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Verified Thrust for given coefficients of lift and drag
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Verified Weight of aircraft for given coefficients of lift and drag
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7 More Thrust Required for Level Unaccelerated Flight Calculators
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Time of Emptying (3)
Created Time of Emptying Circular Horizontal Tank
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Created Time of Emptying Hemispherical Tank
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Created Time of Emptying Tank through Orifice at Bottom
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Torque Required (5)
Created Torque required considering power absorbed in journal bearing
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Created Torque required to overcome Shear Force in Journal Bearing
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Created Torque required to overcome viscous resistance in collar bearing
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Created Torque required to overcome viscous resistance in foot-step bearing
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Created Total torque measured by strain in rotating cylinder method
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Turbulent flow (7)
Created Average height of irregularities for turbulent flow in pipes
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Created Discharge through Pipe given Head Loss in Turbulent Flow
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Created Head Loss due to Friction given Power Required in Turbulent Flow
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Created Power Required to Maintain Turbulent Flow
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Created Roughness Reynold number for turbulent flow in pipes
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Created Shear stress developed for turbulent flow in pipes
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Created Shear velocity for turbulent flow in pipes
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11 More Turbulent flow Calculators
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Valves (3)
Created Intensity of pressure wave produced for gradual closure of valves
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Created Retarding force for gradual closure of valves
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Created Time required to close Valve for Gradual Closure of Valves
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1 More Valves Calculators
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Velocity (5)
Created Angular speed of outer cylinder in rotating cylinder method
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Created Maximum velocity at any Radius using Velocity
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Created Velocity at any radius, radius of pipe, and maximum velocity
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Created Velocity of piston or body for movement of piston in dash-pot
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Created Velocity of sphere in falling sphere resistance method
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Velocity (6)
Created Freestream Velocity for Lift Coefficient in Rotating Cylinder with Circulation
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Created Freestream velocity for lift coefficient with tangential speed
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Created Freestream Velocity for single Stagnation Point
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Created Tangential velocity for single stagnation point
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Created Tangential Velocity of Cylinder with Lift Coefficient
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Created Velocity of Airfoil for Circulation developed on Airfoil
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Velocity of Flow (9)
Created Velocity at Outlet for Head Loss at Exit of Pipe
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Created Velocity at section 1-1 for sudden enlargement
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Created Velocity at section 2-2 for sudden contraction
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Created Velocity at section 2-2 for sudden enlargement
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Created Velocity of Flow at Outlet of Nozzle
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Created Velocity of Flow at outlet of Nozzle for Efficiency and Head
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Created Velocity of Fluid for Head Loss due to Obstruction in Pipe
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Created Velocity of fluid in pipe for head loss at entrance of pipe
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Created Velocity of liquid at vena-contracta
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Velocity of Sound Wave (5)
Created Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
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Created Velocity of Sound Wave given Bulk Modulus
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Created Velocity of sound wave in Mach number for compressible fluid flow
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Created Velocity of Sound Wave using Adiabatic Process
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Created Velocity of Sound Wave using Isothermal Process
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1 More Velocity of Sound Wave Calculators
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Viscosity of Fluid (4)
Created Viscosity of fluid or oil for capillary tube method
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Created Viscosity of fluid or oil for movement of piston in dash-pot
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Created Viscosity of fluid or oil in falling sphere resistance method
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Created Viscosity of fluid or oil in rotating cylinder method
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1 More Viscosity of Fluid Calculators
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Viscous flow (20)
Created Buoyant force in falling sphere resistance method
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Created Density of fluid in falling sphere resistance method
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Created Diameter of capillary tube
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Created Diameter of shaft for speed and shear stress of fluid in journal bearing
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Created Diameter of sphere in falling sphere resistance method
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Created Difference of pressure for viscous flow between two parallel plates
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Created Difference of pressure for viscous or laminar flow
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Created Discharge in capillary tube method
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Created Drag force in falling sphere resistance method
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Created External or outer radius of collar for total torque
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Created Internal or inner radius of collar for total torque
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Created Length for difference of pressure in viscous flow between two parallel plates
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Created Length for pressure head loss in viscous flow between two parallel plates
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Created Length of tube in capillary tube method
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Created Radius of pipe from maximum velocity and velocity at any radius
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Created Radius of shaft for torque required in foot-step bearing
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Created Shear force for torque and diameter of shaft in journal bearing
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Created Shear force or viscous resistance in journal bearing
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Created Shear Stress in Fluid or Oil of Journal Bearing
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Created Speed of rotation for shear force in journal bearing
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Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating (9)
Verified Aerodynamic heating to surface
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Verified Chapman-Rubesin factor
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Verified Coefficient of friction using Stanton equation for incompressible flow
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Verified Density calculation using Chapman-Rubesin factor
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Verified Stanton number for incompressible flow
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Verified Static Density calculation using Chapman-Rubesin factor
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Verified Static viscosity calculation using Chapman-Rubesin factor
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Verified Thermal conductivity using Prandtl number
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Verified Viscosity calculation using Chapman-Rubesin factor
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7 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating Calculators
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