Calculator A to Z

Calculators Created by Sanjay Krishna

Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
https://www.linkedin.com/in/sanjay-krishna-80a7b913b/
299
Formulas Created
200
Formulas Verified
110
Across Categories

List of Calculators by Sanjay Krishna

Following is a combined list of all the calculators that have been created and verified by Sanjay Krishna. Sanjay Krishna has created 299 and verified 200 calculators across 110 different categories till date.
Absolute Temperature (2)
Verified Absolute Temperature for Velocity of Sound Wave in Isothermal Process
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Verified Absolute Temperature for Velocity of Sound Wave using Adiabatic Process
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Aerodynamic Nomenclature (4)
Verified Velocity along roll axis for small sideslip angle
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Verified Velocity along yaw axis for small angle of attack
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Verified Yawing moment
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Verified Yawing moment coefficient
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13 More Aerodynamic Nomenclature Calculators
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Altitude Effects on Power Required and Available (1)
Verified Velocity at Altitude
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6 More Altitude Effects on Power Required and Available Calculators
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Approximate Results Applied to Hypersonic Vehicles (15)
Created Adiabatic wall enthalpy over flat plate using Stanton number
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Created Coefficient of drag over flat under freestream flow conditions
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Created Drag force over flat plate
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Created Free stream enthalpy over flat plate with freestream conditions
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Created Free stream velocity over flat plate using drag force
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Created Free stream velocity over flat plate with freestream conditions
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Created Freestream density over flat plate using Stanton number
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Created Freestream density over flat under freestream flow conditions
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Created Freestream Stanton number for flat plate
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Created Freestream velocity over flat plate using Stanton number
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Created Local heat transfer over flat plate using Stanton number
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Created Pressure ratio for insulated flat plate, strong interaction
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Created Pressure ratio for insulated flat plate, weak interaction
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Created Total enthalpy over flat plate with freestream conditions
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Created Wall enthalpy over flat plate using Stanton number
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Basic Aspects, Boundary Layer Results, and Aerodynamic Heating of Viscous Flow (16)
Created Aerodynamic heating to surface
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Created Chapman-Rubesin factor
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Created Coefficient of friction using Stanton equation for incompressible flow
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Created Density calculation using Chapman-Rubesin factor
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Created Internal Energy for Hypersonic Flow
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Created Non dimensional internal energy parameter
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Created Non dimensional internal energy parameter using wall-to-freestream temperature ratio
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Created Non dimensional static enthalpy
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Created Stanton equation using Overall skin friction coefficient for incompressible flow
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Created Stanton number for incompressible flow
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Created Static Density calculation using Chapman-Rubesin factor
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Created Static enthalpy
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Created Static viscosity calculation using Chapman-Rubesin factor
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Created Thermal conductivity using Prandtl number
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Created Viscosity calculation using Chapman-Rubesin factor
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Created Wall temperature calculation using internal energy change
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Basic Compressible Flow (2)
Verified Ratio of Stagnation and Static Density
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Verified Ratio of Stagnation and Static Temperature
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4 More Basic Compressible Flow Calculators
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Basic Formulas (6)
Verified Coefficient of contraction for sudden contraction
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Verified Difference in liquid level in three compound pipes with same friction coefficient
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Verified Maximum Area of Obstruction in Pipe
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Verified Power Lost ue to Sudden Enlargement
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Verified Power transmission through pipes
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Verified Time taken by pressure wave to travel
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6 More Basic Formulas Calculators
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Basics (2)
Verified Mach Angle
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Verified Mayer's formula
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6 More Basics Calculators
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Basics of HMT (2)
Verified Thermal Conductance for given Thermal Resistance
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Verified Total Thermal Resistance for Conduction through Two Resistances in Parallel
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3 More Basics of HMT Calculators
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Blast-wave part 2 (6)
Created Pressure coefficient combined with blast wave for shuttle
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Created Pressure coefficient combined with blast wave for shuttle at angle of attack
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Created Pressure coefficient for blast wave theory
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Created Pressure coefficient for blast wave theory at very high values of mach
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Created Pressure coefficient for Blunt-nosed cylinder
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Created Pressure coefficient for Blunt-nosed plate
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Bodies connected by string and lying on rough inclined planes (1)
Verified Frictional force on body A
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5 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 Acceleration of system with bodies connected by string and lying on smooth inclined planes
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Verified Tension in string if both bodies are lying on smooth inclined planes
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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 (5)
Verified Acceleration of system with bodies one hanging free, other lying on rough inclined plane
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Verified Coefficient of friction for given tension
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Verified Inclination of plane for given frictional force
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Verified Mass of body B for given frictional force
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Verified Tension in string given coefficient of friction of inclined plane
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2 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 rough horizontal plane (1)
Verified Tension in string given coefficient of friction of horizontal plane
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1 More Bodies connected by string, one hanging free, other lying on rough horizontal plane Calculators
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Bodies connected by string, one hanging free, other lying on smooth inclined plane (3)
Verified Acceleration of system with bodies one hanging free and other lying on smooth inclined plane
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Verified Angle of inclination for given acceleration
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Verified Angle of inclination for given tension
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1 More Bodies connected by string, one hanging free, other lying on smooth inclined plane Calculators
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Body Centered Cubic (3)
Created Atomic Radius in BCC
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Created Lattice Constant of BCC
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Created Total volume of atoms in BCC
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Boundary Layer Flow (10)
Verified Area of surface for average drag coefficient in boundary layer flows
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Verified Distance from leading edge for Blasius's solution in boundary layer flow
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Verified Distance from leading edge in boundary layer flow
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Verified Length of Plate for Reynold number in Laminar Boundary Layer Flow
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Verified Reynold number at end of plate
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Verified Reynold number for drag coefficient in Blasius's solution of boundary layer flow
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Verified Shear Stress at Boundary for Turbulent Boundary Layer over Flat Plate
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Verified Thickness of boundary layer for Blasius's solution in boundary layer flow
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Verified Thickness of boundary layer in boundary layer flow
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Verified Velocity of fluid for Reynold number in Laminar Boundary Layer Flow
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11 More Boundary Layer Flow Calculators
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Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions (20)
Created Adiabatic wall enthalpy using Stanton number
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Created Dynamic viscosity around wall
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Created Enthalpy of wall using Stanton number
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Created Local heat transfer rate using Nusselt's number
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Created Local heat-transfer rate calculation using Stanton number
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Created Local shear stress at wall
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Created Local skin-friction coefficient
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Created Nusselt number for hypersonic vehicle
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Created Nusselt's number with Reynolds number, Stanton number and Prandtl number
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Created Prandtl number with Reynolds number, Nusselt's number, and Stanton number
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Created Reynolds number for given Nusselt's number, Stanton number and Prandtl number
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Created Skin friction coefficient for incompressible flow
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Created Stanton number for hypersonic vehicle
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Created Stanton number with Reynolds number, Nusselt's number, Stanton number and Prandtl number
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Created Static Density equation using skin friction coefficient
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Created Static density equation using Stanton number
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Created Static velocity equation using skin friction coefficient
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Created Static velocity using Stanton number
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Created Static viscosity relation using temperature of wall
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Created Thermal conductivity at edge of boundary layer equation using Nusselt's number
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Buoyancy (3)
Verified Angle of heel for metacentric height in experimental method
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Verified Meta-centric height in experimental method
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Verified Movable weight for metacentric height in experimental method
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8 More Buoyancy Calculators
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Circulation (1)
Verified Circulation for Single Stagnation Point
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3 More Circulation Calculators
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Coefficient of Discharge (1)
Verified Coefficient of Discharge given Time of Emptying Hemispherical Tank
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4 More Coefficient of Discharge Calculators
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Coefficient of Velocity (1)
Verified Coefficient of velocity
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2 More Coefficient of Velocity Calculators
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Coefficient's (2)
Verified Coefficient of drag for sphere in Oseen formula when Reynolds number is between 0.2 and 5
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Verified Coefficient of drag for sphere in stoke's law when Reynolds number is less than 0.2
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3 More Coefficient's Calculators
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Compressible Flow (2)
Verified Pressure ratio for maximum flow rate through nozzle or orifice
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Verified Temperature of fluid for stagnation temperature considering compressible fluid flow
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5 More Compressible Flow Calculators
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Computational-Fluid-Dynamic Solutions (4)
Created Emissivity
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Created Freestream density
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Created Freestream velocity
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Created Reference viscosity
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Conduction (1)
Created Fourier's Law of Heat Conduction
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5 More Conduction Calculators
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Contribution of Aircraft Components- Part 1 (1)
Verified Sidewash angle
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14 More Contribution of Aircraft Components- Part 1 Calculators
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Contribution of Aircraft Components- Part 3 (3)
Verified Dynamic pressure at vertical tail for given vertical tail efficiency
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Verified Dynamic pressure at wing for given vertical tail efficiency
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Verified Vertical tail efficiency
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12 More Contribution of Aircraft Components- Part 3 Calculators
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Crystallography (1)
Created Atomic Packing Factor
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Cutting Force (1)
Created Cutting Force given Thrust Force and Normal Rake Angle
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5 More Cutting Force Calculators
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Cylinders (3)
Verified Total thermal resistance of 2 cylindrical resistances connected in series.
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Verified Total thermal resistance of 3 cylindrical resistances connected in series
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Verified Total Thermal Resistance of Cylindrical wall with Convection on both Sides
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11 More Cylinders Calculators
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Diameter of Pipe (3)
Verified Diameter of pipe for difference in pressure in viscous flow
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Verified Diameter of pipe for head loss due to friction in viscous flow
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Verified Diameter of pipe for loss of pressure head in viscous flow
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1 More Diameter of Pipe Calculators
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Discharge (3)
Verified Discharge in Borda's Mouthpiece Running Free
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Verified Discharge in Borda's Mouthpiece Running Full
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Verified Discharge in Convergent-Divergent Mouthpiece
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3 More Discharge Calculators
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Discharge (1)
Verified Coefficient of Discharge for Time required to Empty Reservoir
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12 More Discharge Calculators
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Drag during Level Unaccelerated Flight (2)
Verified Coefficient of Drag for given thrust and weight
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Verified Lift-induced 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 (2)
Verified Drag Force for body moving in Fluid of Certain Density
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Verified Total Drag force on Sphere
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5 More Drag Force on Body Calculators
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Dynamics of Fluid Flow (4)
Verified Actual discharge in venturimeter
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Verified Difference in pressure head for heavier liquid in manometer
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Verified Difference in pressure head for light liquid in manometer
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Verified Velocity at any point for coefficient of pitot-tube
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3 More Dynamics of Fluid Flow Calculators
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Elements of Kinetic Theory (15)
Created Emissivity per unit mole
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Created Kinetic energy per mole
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Created Kinetic energy per mole using molar volume
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Created Kinetic energy per mole using temperature of gas
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Created Mean free path of single-species gas
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Created Mean free path using number density
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Created Molar volume using kinetic energy per mole
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Created Number density
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Created Pressure of gas using number density
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Created Pressure using kinetic energy per mole
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Created Pressure using molar volume
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Created Specific gas constant using kinetic energy per mole
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Created Temperature of gas using Emissivity per unit mole
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Created Temperature of gas using kinetic energy per mole
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Created Volume of gas
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Elevator and Stick Deflection Angles (1)
Verified Elevator deflection angle for given gearing ratio
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3 More Elevator and Stick Deflection Angles Calculators
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Enthalpy and Velocity (5)
Verified Enthalpy ahead of normal shock from normal shock energy equation
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Verified Enthalpy behind of normal shock from normal shock energy equation
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Verified Velocity ahead of normal shock by normal shock momentum equation
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Verified Velocity behind of normal shock by normal shock momentum equation
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Verified Velocity upstream of shock using Prandtl relation
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6 More Enthalpy and Velocity Calculators
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Face Centered Crystal (3)
Created Atomic Radius in FCC
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Created Lattice Constant of FCC
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Created Volume of atoms in FCC
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Flight Envelope (2)
Verified Lift Coefficient for given wing loading and turn radius
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Verified Wing loading for given turn radius
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14 More Flight Envelope Calculators
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Flow in Open Channels (12)
Verified Bazin's constant
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Verified Chezy's constant considering Bazin formula
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Verified Chezy's constant considering velocity
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Verified Critical depth considering flow in open channels
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Verified Critical depth considering minimum specific energy
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Verified Critical Depth using Critical Velocity
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Verified Critical velocity considering flow in open channels
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Verified Discharge per unit width considering flow in open channels
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Verified Hydraulic mean depth considering Bazin formula
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Verified Hydraulic mean depth using Chezy's formula
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Verified Minimum Specific Energy using Critical Depth
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Verified Velocity of Chezy's formula
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7 More Flow in Open Channels Calculators
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Gearing Ratio (1)
Verified Control stick length for given gearing ratio
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3 More Gearing Ratio Calculators
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Gliding Flight (2)
Verified Lift force for given glide angle
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Verified Lift-to-drag ratio for given glide angle
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3 More Gliding Flight Calculators
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Head Available (3)
Verified Head available at Base of Nozzle
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Verified Total head at inlet of pipe for head available at base of nozzle
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Verified Total head available at inlet of pipe for efficiency of power transmission
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Hinge Moment (1)
Verified Hinge moment coefficient for given stick force
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2 More Hinge Moment Calculators
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Hypersonic Equivalence Principle and Blast-Wave Theory (16)
Created Blunt-nosed flat plate pressure ratio (first approximation)
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Created Boltzmann constant for cylindrical blast wave
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Created Coefficient of drag equation using energy released from blast wave
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Created Creation pressure for planar blast wave
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Created Energy for blast wave
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Created Modified Energy for cylindrical blast wave
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Created Modified pressure equation for cylindrical blast wave
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Created Modified Radial coordinate equation for cylindrical blast wave
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Created Pressure for cylindrical blast wave
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Created Pressure ratio for blunt cylinder blast wave
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Created Pressure ratio for blunt slab blast wave
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Created Radial coordinate for planar blast wave
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Created Radial coordinate of blunt slab blast wave
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Created Radial coordinate of cylindrical blast wave
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Created Simplified pressure ratio for blunt cylinder blast wave
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Created Time required for blast wave
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Hypersonic Flight Paths: Velocity-Altitude Map (9)
Created Blunt-nosed radial coordinate flat plate (first approximation)
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Created Forces acting on body along flight path
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Created Forces acting Perpendicular to body on flight path
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Created Pressure ratio of Blunt-nosed cylinder (first approximation)
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Created Radial coordinate of Blunt-nosed cylinder (first approximation)
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Created Radius for cylinder-wedge body shape
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Created Radius for sphere-cone body shape
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Created Radius of curvature for cylinder wedge body shape
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Created Radius of curvature for sphere cone body shape
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Hypersonic Inviscid Flowfields: Approximate Methods (11)
Created Non dimensional radius for hypersonic vehicles
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Created Non-dimensional density
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Created Non-dimensional density for high mach number
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Created Non-dimensional parallel velocity component for high mach number
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Created Non-dimensional perpendicular velocity component for high mach number
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Created Non-dimensional pressure
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Created Non-dimensional pressure for high mach number
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Created Slenderness ratio with cone radius for hypersonic vehicle
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Created Transformed conical variable
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Created Transformed conical variable with cone angle in hypersonic flow
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Created Transformed conical variable with wave angle
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Hypersonic Inviscid Flowfields: Exact Methods (18)
Created Density before shock formation for compression wave
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Created Density before Shock formation for Expansion Wave
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Created Detachment distance of cylinder wedge body shape
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Created Detachment distance of sphere cone body shape
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Created Grid point calculation for shock waves
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Created Local shock velocity equation
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Created Mach wave behind shock
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Created Mach wave behind shock with mach infinity
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Created New pressure after shock formation for compression wave
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Created New pressure after shock formation, subtracted to velocity for expansion wave
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Created Nose radius of cylinder-wedge
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Created Nose radius of sphere cone
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Created Pressure ratio for unsteady waves
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Created Pressure ratio for unsteady waves with subtracted induced mass motion for expansion waves
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Created Ratio of new and old temperature
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Created Ratio of new and old temperature for expansion waves
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Created Temperature ratio for unsteady compression waves
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Created Temperature ratio for unsteady expansion wave
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Hypersonic Small-Disturbance Equations (17)
Created Change in velocity for hypersonic flow in x direction
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Created Coefficient of pressure with slenderness ratio
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Created Coefficient of pressure with slenderness ratio and similarity constant
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Created Constant g used for finding location of perturbed shock
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Created Density ratio with similarity constant having slenderness ratio
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Created Distance from tip of leading edge to base
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Created Doty and Rasmussen - normal-force coefficient
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Created Inverse of density for hypersonic flow
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Created Inverse of density for hypersonic flow using Mach number
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Created Non dimensional Change in hypersonic disturbance velocity in x direction
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Created Non dimensional Change in hypersonic disturbance velocity in y direction
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Created Non dimensional pressure equation with slenderness ratio
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Created Non dimensional Velocity disturbance in y direction in hypersonic flow
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Created Non- dimensionalised time
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Created Rasmussen closed form expression for shock wave angle
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Created Similarity constant equation using wave angle
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Created Similarity constant equation with slenderness ratio
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Hypersonic Transition (16)
Created Boundary-layer momentum thickness using Reynolds number at transition point
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Created Eddy viscosity calculation
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Created Local Mach Number using Reynolds number equation at transition region
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Created Location of transition point
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Created Prandtl number of transition flow
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Created Reynolds number equation using boundary-layer momentum thickness
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Created Reynolds number equation using local Mach number
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Created Specific heat at constant pressure for transient flow
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Created Static density at transition point
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Created Static density equation using boundary-layer momentum thickness
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Created Static velocity at transition point
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Created Static velocity using boundary-layer momentum thickness
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Created Static viscosity at transition point
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Created Static viscosity equation using boundary-layer momentum thickness
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Created Thermal conductivity of transition flow
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Created Transition Reynolds number
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Hypersonic Viscous Interactions (18)
Created Large Mach number over flat plate using static temperature and wall temperature
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Created Mach number over flat plate using static temperature and wall temperature
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Created Pressure Ratio for Cold-Wall case Strong Interaction
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Created Pressure Ratio for Cold-Wall case Weak Interaction
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Created Static density of fluid over flat plate
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Created Static temperature of fluid over flat plate
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Created Static temperature of plate using wall viscosity
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Created Static temperature over flat plate under viscous, very high Mach flow
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Created Static temperature over flat plate using Static Mach Number
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Created Static viscosity using wall temperature and static temperature
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Created Total temperature over flat plate under viscous Mach flow
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Created Total temperature over flat plate under viscous very high Mach flow
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Created viscosity of wall using wall temperature and static temperature
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Created Wall density of fluid over flat plate
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Created Wall Temperature of Fluid over Flat Plate
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Created Wall temperature of plate using wall viscosity
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Created Wall temperature over flat plate under viscous, very high Mach flow
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Created Wall temperature over flat plate using Static Mach Number
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Ideal flow or Potential flow (1)
Verified Radius of Rankine circle
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13 More Ideal flow or Potential flow Calculators
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Incompressible flow over airfoil (4)
Verified Boundary layer thickness for Turbulent flow
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Verified Center of pressure location for cambered airfoil
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Verified Skin friction drag coefficient for flat plate in laminar flow
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Verified Skin friction drag coefficient for flat plate in Turbulent flow
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4 More Incompressible flow over airfoil Calculators
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Introduction (1)
Verified Diameter of pipe from maximum velocity and velocity at any radius
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18 More Introduction Calculators
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Introduction (2)
Verified Airspeed measurement by Pitot Tube for Low-Speed Incompressible Flow
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Verified Lift per unit Span by Kutta-Joukowski theorem
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14 More Introduction Calculators
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Kinematics of Flow (3)
Verified Height or depth of paraboloid for volume of air
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Verified Total Pressure Force at Bottom of Cylinder
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Verified Total pressure force on top of cylinder
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4 More Kinematics of Flow Calculators
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Laminar Boundary Layer at Stagnation point on Blunt body (7)
Created Newtonian Dynamic pressure
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Created Newtonian Pressure distribution over Surface using Cosine Angle
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Created Nusselt number at stagnation point
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Created Nusselt number for stagnation point on blunt body
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Created Reynolds analogy factor in Finite deference method
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Created Reynolds analogy for Stanton number in finite difference method
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Created Stagnation pressure
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Landing Performance (1)
Verified Landing ground roll distance
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3 More Landing Performance Calculators
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Length of Pipe (3)
Verified Length of pipe for difference of pressure in viscous flow
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Verified Length of pipe for head loss due to friction in viscous flow
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Verified Length of pipe for loss of pressure head in viscous flow
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Longitudinal Control of Elevator Hinge Moment (1)
Verified Flight velocity for given elevator hinge moment coefficient
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4 More Longitudinal Control of Elevator Hinge Moment Calculators
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Loss of Head (2)
Verified Loss of head due to friction
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Verified Loss of pressure head for viscous flow through circular pipe
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1 More Loss of Head Calculators
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Loss of Head (3)
Verified Head Loss due to Friction for Efficiency of Power Transmission
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Verified Loss of head at exit of pipe
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Verified Loss of head due to obstruction in pipe
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5 More Loss of Head Calculators
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Merchant Force Circle (Mechanics of Orthogonal metal cutting) (7)
Created Area of shear plane for given shear angle, width of cut and uncut chip thickness
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Created Coefficient of friction for given friction angle
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Created Coefficient of friction for given thrust force, cutting force and normal rake angle
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Created Coefficient of Friction given Forces Normal and along Tool Rake Face
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Created Force acting Normal to Rake Face given Cutting Force and Thrust Force
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Created Side cutting edge angle for given width of cut
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Created Width of cut for given side cutting edge angle
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15 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
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Modern design-oriented code (2)
Created Convective heat transfer to surface
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Created Radiative heat transfer to surface stemming from thermal radiation
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Newtonian Flow (14)
Created Coefficient of drag equation with angle of attack
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Created Coefficient of drag equation with coefficient of normal force
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Created Coefficient of lift equation with angle of attack
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Created Coefficient of lift equation with coefficient of normal force
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Created Drag force with angle of attack
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Created Exact normal shock wave maximum coefficient of pressure
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Created Force Exerted on Surface given Static Pressure
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Created Lift force with angle of attack
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Created Mass Flux Incident on Surface Area
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Created Maximum Pressure coefficient
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Created Modified Newtonian Law
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Created Pressure coefficient for slender 2D bodies
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Created Pressure coefficient for slender bodies of revolution
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Created Time rate of change of momentum of mass flux
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Normal Shock Waves (4)
Verified Characteristic Mach number
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Verified Critical speed of sound from Prandtl relation
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Verified Mach Number behind Shock
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Verified Prandtl Condition
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16 More Normal Shock Waves Calculators
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Notches and Weirs (2)
Verified Length of Crest of Weir or Notch
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Verified Time required to Empty Reservoir
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4 More Notches and Weirs Calculators
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Oblique Shock and Expansion Waves (1)
Verified Component of Upstream Mach normal to oblique shock
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18 More Oblique Shock and Expansion Waves Calculators
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Oblique Shock Relation (15)
Created Coefficient of pressure derived from oblique shock theory
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Created Density ratio when Mach become infinite
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Verified Dynamic pressure for given specific heat ratio and Mach number
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Created Exact Density Ratio
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Created Exact pressure ratio
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Created Non-dimensional pressure coefficient
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Created Parallel upstream flow components after shock as Mach tends to infinite
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Created Perpendicular Upstream Flow Components behind Shock Wave
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Created Pressure Coefficient behind Oblique Shock Wave
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Created Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number
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Created Pressure ratio when Mach becomes infinite
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Created Temperature ratio when Mach becomes infinite
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Created Temperature ratios
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Created Velocity of sound using dynamic pressure and density
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Created Wave angle for small deflection angle
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Orifices and Mouthpieces (8)
Verified Area at vena contracta for discharge and constant head
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Verified Area of Mouthpiece in Borda's Mouthpiece Running Free
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Verified Area of Mouthpiece in Borda's Mouthpiece Running Full
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Verified Area of Orifice given Time of Emptying Hemispherical Tank
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Verified Coefficient of Contraction given Area of Orifice
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Verified Head of Liquid above Centre of Orifice
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Verified Horizontal distance for coefficient of velocity and vertical distance
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Verified Vertical distance for coefficient of velocity and horizontal distance
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8 More Orifices and Mouthpieces Calculators
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Parameters (19)
Created Axial force coefficient
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Created Coefficient of drag
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Created Coefficient of pressure with similarity parameters
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Created Deflection angle
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Created Drag force
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Created Dynamic pressure
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Created Dynamic Pressure given Coefficient of Lift
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Created Hypersonic similarity parameter
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Created Lift coefficient
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Created Lift Force
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Created Mach number with fluids
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Created Mach ratio at high mach number
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Created Moment coefficient
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Created Newtonian sine squared law for pressure coefficient
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Created Normal Force Coefficient
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Created Pressure ratio for high Mach number
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Created Pressure ratio having high mach number with similarity constant
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Created Shear-stress distribution.
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Created Supersonic expression for pressure coefficient on surface with local deflection angle
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1 More Parameters Calculators
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Plane Walls (2)
Verified Interface temperature of composite wall of 2 layers given outer surface temperature
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Verified Total Thermal Resistance of Plane Wall with Convection on both Sides
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20 More Plane Walls Calculators
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Power Available and Maximum Velocity (1)
Verified Shaft brake power for reciprocating engine-propeller combination
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2 More Power Available and Maximum Velocity Calculators
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Power Required for Level Unaccelerated Flight (3)
Verified Power required for given aerodynamic coefficients
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Verified Thrust of aircraft required for given required power
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Verified Weight of aircraft for given required power
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7 More Power Required for Level Unaccelerated Flight Calculators
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Power Transmission Efficiency (1)
Verified Efficiency of power transmission in flow through pipes
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2 More Power Transmission Efficiency Calculators
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Pressure (4)
Verified Pressure at upstream point on streamline by Bernoulli's equation
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Verified Pressure Coefficient
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Verified Static pressure in incompressible flow
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Verified Surface pressure coefficient for non-lifting flow over circular cylinder
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9 More Pressure Calculators
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Pressure and Density (1)
Verified Density of fluid considering velocity at outlet of orifice
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3 More Pressure and Density Calculators
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Radial Velocity (1)
Verified Radial velocity for non-lifting flow over circular cylinder
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2 More Radial Velocity Calculators
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Range and Endurance of Jet Airplane (5)
Verified Endurance for given Lift-to-Drag ratio of Jet Airplane
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Verified Lift-to-Drag ratio for given Endurance of Jet Airplane
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Verified Range of Jet Airplane
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Verified Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane
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Verified Thrust-Specific Fuel Consumption for given Range of Jet Airplane
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3 More Range and Endurance of Jet Airplane Calculators
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Range and Endurance of Propeller-Driven Airplane (1)
Verified Lift-to-Drag ratio for given Range of Propeller-Driven Airplane
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9 More Range and Endurance of Propeller-Driven Airplane Calculators
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Rate of Climb (3)
Verified Rate of Climb
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Verified Rate of Climb for given excess power
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Verified Weight of aircraft for given excess power
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7 More Rate of Climb Calculators
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Reference Temperature Method (15)
Created Chord length for flat plate case
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Created Local Reynolds number
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Created Local turbulent skin-friction coefficient for incompressible flow
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Created Mach number at reference temperature
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Created Overall skin-friction drag coefficient
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Created Overall skin-friction drag coefficient for incompressible flow
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Created Reference temperature equation
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Created Reynolds number for chord length
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Created Reynolds number for chord length using Overall skin-friction drag coefficient
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Created Stanton Number obtained from classical theory
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Created Static density of plate using chord length for flat plate case
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Created Static velocity of plate using chord length for flat plate case
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Created Static viscosity of plate using chord length for flat plate case
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Created Turbulent flat-plate skin-friction coefficient
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Created Wall temperature using reference temperature
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Simple Cubic Cell (3)
Created Atomic Radius in SCC
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Created Lattice Constant of SCC
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Created Total volume of atoms in SCC
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Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations (11)
Created Coefficient of pressure equation using specific heat ratio
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Created curvilinear grid location equation
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Created Density equation using enthalpy and pressure
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Created Enthalpy equation using coefficient of pressure for calorically perfect gas
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Created Enthalpy equation using pressure and density
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Created Enthalpy equation using specific heat ratio
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Created Free stream enthalpy
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Created local shock-layer thickness
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Created pressure equation using Enthalpy and density
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Created total enthalpy equation using specific heat ratio and velocities
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Created Total specific enthalpy
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Spheres (2)
Verified Heat flow rate through spherical wall
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Verified Thermal Resistance of Spherical Wall
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9 More Spheres Calculators
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Stagnation Points (1)
Verified Radius of Cylinder for Single Stagnation Point
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3 More Stagnation Points Calculators
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Stagnation Temperature (1)
Verified Stagnation Temperature considering Compressible Fluid Flow
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1 More Stagnation Temperature Calculators
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Stick Forces (2)
Verified Elevator chord length for given stick force
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Verified Elevator Stick force for given gearing ratio
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5 More Stick Forces Calculators
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Stream Function (2)
Verified Stream function for flow over Rankine oval
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Verified Stream function for uniform incompressible flow in polar coordinates
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7 More Stream Function Calculators
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Tail Contribution (2)
Verified Angle of incidence of wing
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Verified Mean aerodynamic chord for given tail pitching moment coefficient
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19 More Tail Contribution Calculators
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Tail Contribution Contd (4)
Verified Horizontal tail volume ratio for given pitching moment coefficient
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Verified Tail Efficiency for given tail volume ratio
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Verified Tail lift coefficient for given tail volume ratio
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Verified Tail Pitching moment coefficient for given tail volume ratio
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10 More Tail Contribution Contd Calculators
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Takeoff Performance (1)
Verified Liftoff velocity for given stall velocity
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13 More Takeoff Performance Calculators
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Tangential Velocity (2)
Verified Tangential velocity for 2-D Vortex flow
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Verified Tangential velocity for lifting flow over circular cylinder
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1 More Tangential Velocity Calculators
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Thrust Force (2)
Created Thrust force for given frictional force along tool rake face, cutting force and normal rake angle
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Created Thrust Force given Cutting Force and Normal Rake Angle
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2 More Thrust Force Calculators
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Thrust Required for Level Unaccelerated Flight (2)
Verified Minimum Thrust required for given weight
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Verified Thrust-to-weight ratio
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10 More Thrust Required for Level Unaccelerated Flight Calculators
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Time of Emptying (1)
Verified Time of Emptying Hemispherical Tank
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2 More Time of Emptying Calculators
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Torque Required (1)
Verified Total torque measured by strain in rotating cylinder method
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4 More Torque Required Calculators
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Turbulent Flow (2)
Verified Shear stress developed for turbulent flow in pipes
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Verified Shear velocity for turbulent flow in pipes
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16 More Turbulent Flow Calculators
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Turning Flight (1)
Verified Weight of aircraft during level turn
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11 More Turning Flight Calculators
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Valves (1)
Verified Retarding force for gradual closure of valves
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3 More Valves Calculators
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Velocity (4)
Verified Angular speed of outer cylinder in rotating cylinder method
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Verified Maximum velocity at any Radius using Velocity
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Verified Velocity at any radius given radius of pipe, and maximum velocity
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Verified Velocity of piston or body for movement of piston in dash-pot
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1 More Velocity Calculators
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Velocity (2)
Verified Freestream Velocity for single Stagnation Point
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Verified Tangential velocity for single stagnation point
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4 More Velocity Calculators
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Velocity of Flow (3)
Verified Velocity at Outlet for Head Loss at Exit of Pipe
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Verified Velocity of Fluid for Head Loss due to Obstruction in Pipe
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Verified Velocity of liquid at vena-contracta
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6 More Velocity of Flow Calculators
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Velocity of Sound Wave (2)
Verified Velocity of Sound Wave using Adiabatic Process
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Verified Velocity of Sound Wave using Isothermal Process
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4 More Velocity of Sound Wave Calculators
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Velocity Potential (3)
Verified Velocity potential for 2-D doublet flow
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Verified Velocity potential for 2-D source flow
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Verified Velocity potential for uniform incompressible flow in polar coordinates
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2 More Velocity Potential Calculators
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Viscosity of Fluid (2)
Verified Viscosity of fluid or oil for movement of piston in dash-pot
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Verified Viscosity of fluid or oil in rotating cylinder method
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3 More Viscosity of Fluid Calculators
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Viscous Flow (15)
Created Adiabatic wall enthalpy for flat plate
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Created Adiabatic wall enthalpy using recovery factor
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Created Aerodynamic Heating Equation for Stanton number
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Created Coefficient of friction using Stanton number for flat plat case
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Created Drag per unit span
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Created Prandtl number for flat plate with viscous flow
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Created Recovery factor calculation using Prandtl number
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Created Recovery factor for flat plate with viscous flow
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Created Recovery Factor using temperature
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Created Skin-friction drag Coefficient
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Created Skin-friction drag for flat plate in viscous flow
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Created Stanton number with coefficient of friction
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Created Static density equation using aerodynamic equation
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Created Static velocity equation using aerodynamic heating equation
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Created Total enthalpy in inviscid flow outside boundary layer
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