Calculators Created by Maiarutselvan V

Verified Normal force coefficient with aerodynamic normal force

Go

Verified Rolling moment

Go

Verified Rolling moment coefficient

Go

Verified Velocity along pitch axis for small sideslip angle

Go

Verified Velocity along roll axis for small angle of attack

Go

12 More Aerodynamic Nomenclature Calculators

Go

Created Angle of attack for circulation developed on the airfoil

Go

Created Angle of attack for lift coefficient on the airfoil

Go

Created Chord length for circulation developed on the airfoil

Go

Verified Power required at an altitude

Go

Verified Power required at an altitude for given power required at sea-level condition

Go

5 More Altitude Effects on Power Required and Available Calculators

Go

Verified Coefficient of drag over flat under freestream flow conditions

Go

Verified Drag force over flat plate

Go

Verified Freestream Stanton number for flat plate

Go

Verified Local heat transfer over flat plate using Stanton number

Go

Verified Pressure ratio for insulated flat plate, the weak interaction

Go

10 More Approximate Results Applied to Hypersonic Vehicles Calculators

Go

Verified Ratio of stagnation and static pressure

Go

5 More Basic Compressible Flow Calculators

Go

Verified Friction Coefficient

Go

Verified Mach Number

Go

Verified Stagnation Temperature

Go

5 More Basics Calculators

Go

Verified Pressure coefficient for blast wave theory

Go

5 More Blast-wave part 2 Calculators

Go

Verified Acceleration of system for given mass of body A

Go

Verified Acceleration of system for given mass of body B

Go

Verified Frictional force on body B

Go

Verified Tension in string for given mass of body A

Go

Verified Tension in string for given mass of body B

Go

1 More Bodies connected by string and lying on rough inclined planes Calculators

Go

Verified Angle of inclination of plane with body A

Go

Verified Angle of inclination of plane with body B

Go

2 More Bodies connected by string and lying on smooth inclined planes Calculators

Go

Verified Coefficient of friction for given frictional force

Go

Verified Frictional force

Go

5 More Bodies connected by string, one hanging free, other lying on a rough inclined plane Calculators

Go

Verified Tension in string when one body is lying on smooth inclined plane

Go

3 More Bodies connected by string, one hanging free, other lying on smooth inclined plane Calculators

Go

Created Area of surface for average drag coefficient in boundary layer flows

Go

Created Average coefficient of drag for drag force in boundary layer flows

Go

Created Coefficient of drag for Blasius's solution in boundary layer flow

Go

Created Coefficient of drag for Reynold number in the laminar boundary layer flow

Go

Created Distance from leading edge for Blasius's solution in boundary layer flow

Go

Created Distance from leading edge in boundary layer flow

Go

Created Drag force for average drag coefficient in boundary layer flows

Go

Created Drag force on the plate in boundary layer flow

Go

Created Freestream velocity for local drag coefficient in boundary layer flows

Go

Created Length of the plate for Reynold number in the laminar boundary layer flow

Go

Created Local drag coefficient for shear stress in boundary layer flows

Go

Created Reynold number at the end of the plate

Go

Created Reynold number for drag coefficient in Blasius's solution of boundary layer flow

Go

Created Reynold number for drag force on the plate in boundary layer flow

Go

Created Shear stress at the boundary for turbulent boundary layer over a flat plate

Go

Created Shear stress for local drag coefficient in boundary layer flows

Go

Created Thickness of boundary layer for Blasius's solution in boundary layer flow

Go

Created Thickness of boundary layer in boundary layer flow

Go

Created Velocity of fluid for Reynold number in the laminar boundary layer flow

Go

Created Viscosity of liquid for drag force on the plate in boundary layer flow

Go

Created Width of the plate for drag force on the plate in boundary layer flow

Go

Verified Dynamic viscosity around wall

Go

Verified Local heat transfer rate using Nusselt's number

Go

Verified Local heat-transfer rate calculation using Stanton number

Go

Verified Local shear stress at wall

Go

Verified Nusselt's number with Reynolds number, Stanton number and Prandtl number

Go

Verified Prandtl number with Reynolds number, Nusselt's number, and Stanton number

Go

Verified Stanton number for hypersonic vehicle

Go

Verified Static Density equation using skin friction coefficient

Go

Verified Static density equation using Stanton number

Go

Verified Static velocity equation using skin friction coefficient

Go

Verified Static velocity using Stanton number

Go

Verified Static viscosity relation using temperature of wall

Go

Verified Thermal conductivity at edge of boundary layer equation using Nusselt's number

Go

7 More Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions Calculators

Go

Created Angle of heel for metacentric height in experimental method

Go

Created Centre of Buoyancy

Go

Created Meta-centric height for time period of oscillation and radius of gyration

Go

Created Meta-centric height in experimental method

Go

Created Movable weight for metacentric height in experimental method

Go

Created Radius of gyration for metacentric height and time period of oscillation

Go

Created Time period of oscillation in the ship

Go

Created Volume of body in fluid for metacentric height and BG

Go

Created Volume of fluid displaced

Go

Created Circulation developed on the airfoil

Go

Created Circulation for a single stagnation point

Go

Created Circulation for lift force on a cylinder

Go

Created Circulation in the location of stagnation points

Go

1 More Circulation Calculators

Go

Created Coefficient of discharge

Go

Created Coefficient of discharge considering time for emptying a tank

Go

Created Coefficient of discharge considering time of emptying a circular horizontal tank

Go

Created Coefficient of discharge considering time of emptying a hemispherical tank

Go

Created Coefficient of discharge for area and velocity

Go

Created Coefficient of velocity

Go

Created Coefficient of velocity for horizontal and vertical distance

Go

Created Coefficient of velocity for the head of liquid and head loss

Go

Created Coefficient of drag for sphere in Oseen formula when Reynolds number is between 0.2 and 5

Go

Created Coefficient of drag for sphere in stoke's law when Reynolds number is less than 0.2

Go

Created Coefficient of lift for an airfoil

Go

Created Lift coefficient for a rotating cylinder with circulation

Go

Created Lift coefficient for a rotating cylinder with tangential speed

Go

Created Lift coefficient for lift force in body moving on fluid

Go

Created Absolute temperature for the velocity of sound wave in the isothermal process

Go

Created Absolute temperature for velocity of sound wave in terms of adiabatic process

Go

Created Bulk modulus for the velocity of sound wave

Go

Created Density of fluid considering velocity at outlet of orifice

Go

Created Density of the fluid for stagnation considering compressible fluid flow

Go

Created Mach angle for the compressible fluid flow

Go

Created Mach number for the compressible fluid flow

Go

Created Pressure at inlet considering maximum flow rate of fluid

Go

Created Pressure at inlet of the tank or vessel considering compressible fluid flow

Go

Created Pressure ratio for maximum flow rate through nozzle or orifice

Go

Created Temperature of fluid for stagnation temperature considering compressible fluid flow

Go

Created Velocity at the outlet of the nozzle for maximum flow rate of fluid

Go

Created Velocity of fluid considering the Mach angle in the compressible fluid flow

Go

Verified Emissivity

Go

Verified Reference viscosity

Go

2 More COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS Calculators

Go

Verified Sideslip angle for an Aircraft

Go

14 More Contribution of Aircraft Components- Part 1 Calculators

Go

Verified Wing area for given moment produced by vertical tail

Go

Verified Wing dynamic pressure for given yawing moment coefficient

Go

Verified Wingspan for given yawing moment coefficient

Go

11 More Contribution of Aircraft Components- Part 2 Calculators

Go

Created Cutting force for frictional force along the tool rake face, thrust force and normal rake angle

Go

Created Cutting force for given force along the shear force, thrust force, and shear angle

Go

4 More Cutting Force Calculators

Go

Verified Convection resistance for a cylindrical layer

Go

Verified Length of cylindrical wall for given heat flow rate

Go

12 More Cylinders Calculators

Go

Created Diameter of pipe for difference in pressure in viscous flow

Go

Created Diameter of pipe for head loss due to friction in viscous flow

Go

Created Diameter of pipe for loss of pressure head in viscous flow

Go

Created Discharge In Borda's mouthpiece running free

Go

Created Discharge In Borda's mouthpiece running full

Go

Created Discharge in the convergent-divergent mouthpiece

Go

Created Discharge through fully sub-merged orifice

Go

Created Discharge through large rectangular orifice

Go

Created Discharge through partially sub-merged orifice

Go

Created Coefficient of discharge for time required to empty a reservoir

Go

Created Discharge over a broad-crested weir

Go

Created Discharge over a broad-crested weir for head of liquid at middle

Go

Created Discharge over a broad-crested weir with velocity approach

Go

Created Discharge over a trapezoidal notch or weir

Go

Created Discharge over a triangular notch or weir

Go

Created Discharge over rectangle notch or weir

Go

Created Discharge over rectangle weir considering Bazin's formula

Go

Created Discharge over rectangle weir considering Francis's formula

Go

Created Discharge over rectangle weir for Bazin's formula with velocity approach

Go

Created Discharge over rectangle weir with two end contractions

Go

Created Discharge with velocity of approach

Go

Created Discharge without velocity of approach

Go

Verified Zero-lift drag coefficient at minimum required thrust

Go

Verified Zero-lift drag coefficient for given required thrust

Go

5 More Drag during Level Unaccelerated Flight Calculators

Go

Created Drag force for a body moving in a fluid of certain density

Go

Created Pressure drag from total drag force on a sphere

Go

Created Skin friction drag from total drag force on a sphere

Go

Created Total drag force on a sphere

Go

3 More Drag Force on Body Calculators

Go

Created Actual discharge in venturimeter

Go

Created Coefficient of pitot-tube for velocity at any point

Go

Created Difference in pressure head for heavier liquid in manometer

Go

Created Difference in pressure head for light liquid in manometer

Go

Created Resultant bend force along x and y direction

Go

Created Velocity at any point for coefficient of pitot-tube

Go

Verified Emissivity per unit mole

Go

Verified Kinetic energy per mole

Go

Verified Kinetic energy per mole using molar volume

Go

Verified Kinetic energy per mole using temperature of gas

Go

Verified Mean free path of single-species gas

Go

Verified Pressure using kinetic energy per mole

Go

Verified Pressure using molar volume

Go

Verified Specific gas constant using kinetic energy per mole

Go

Verified Temperature of gas using Emissivity per unit mole

Go

Verified Temperature of gas using kinetic energy per mole

Go

5 More ELEMENTS OF KINETIC THEORY Calculators

Go

Verified Stick deflection angle for given stick force

Go

3 More Elevator and Stick Deflection Angles Calculators

Go

Verified Static enthalpy behind normal shock for given upstream enthalpy and Mach number

Go

Verified Static enthalpy ratio across normal shock

Go

9 More Enthalpy and Velocity Calculators

Go

Verified Aerodynamic Heating Equation for Stanton number

Go

Verified Coefficient of friction using Stanton number for flat plat case

Go

Verified Drag per unit span

Go

Verified Prandtl number for flat plate with viscous flow

Go

Verified Recovery Factor using temperature

Go

Verified Skin-friction drag for flat plate in viscous flow

Go

Verified Static density equation using aerodynamic equation

Go

Verified Static velocity equation using aerodynamic heating equation

Go

7 More Flat-Plate for Viscous flow case Calculators

Go

Verified Load factor for given turn radius for high-performance fighter aircraft

Go

Verified Turn radius for high load factor

Go

Verified Turn rate for given lift coefficient

Go

Verified Velocity for given turn radius for a high load factor

Go

12 More Flight Envelope Calculators

Go

Created Area of flow for a circular channel

Go

Created Bazin's constant

Go

Created Chezy's constant considering Bazin formula

Go

Created Chezy's constant considering Kutter's formula

Go

Created Chezy's constant considering Manning's formula

Go

Created Chezy's constant considering velocity

Go

Created Critical depth considering flow in open channels

Go

Created Critical depth considering minimum specific energy

Go

Created Critical depth considering the critical velocity

Go

Created Critical velocity considering flow in open channels

Go

Created Discharge per unit width considering flow in open channels

Go

Created Hydraulic mean depth considering Bazin formula

Go

Created Hydraulic mean depth considering Manning's formula

Go

Created Hydraulic mean depth using Chezy's formula

Go

Created Manning's coefficient or constant

Go

Created Minimum specific energy considering the critical depth

Go

Created Radius of a circular channel considering wetted perimeter

Go

Created Velocity of Chezy's formula

Go

Created Wetted perimeter for a circular channel

Go

Created Area of the nozzle at outlet for maximum power transmission through nozzle

Go

Created Area of the pipe for maximum power transmission through nozzle

Go

Created Coefficient of contraction for sudden contraction

Go

Created Diameter of nozzle for maximum power transmission through nozzle

Go

Created Diameter of the equivalent pipe

Go

Created Difference in liquid level in three compound pipes with same friction coefficient

Go

Created Discharge in the equivalent pipe

Go

Created Intensity of pressure wave produced for gradual closure of valves

Go

Created Length of pipe for maximum power transmission through nozzle

Go

Created Length of the equivalent pipe

Go

Created Maximum area of obstruction in the pipe

Go

Created Power lost due to sudden enlargement

Go

Created Power transmission through pipes

Go

Created Retarding force for gradual closure of valves

Go

Created Time required to close the valve for gradual closure of valves

Go

Created Time taken by pressure wave to travel

Go

5 More Flow through pipes Calculators

Go

Created Force along shear force for given force normal to shear force, shear, friction & normal rake angles

Go

Created Force along the shear force for given cutting force, thrust force, and shear angle

Go

1 More Force Along The Shear Calculators

Go

Created Force normal to shear force for given cutting force, thrust force, and shear angle

Go

2 More Force Normal To Shear Calculators

Go

Verified 2-D Lift coefficient for cylinder

Go

Verified Airspeed measurement by venturi

Go

Verified Freestream density by Kutta-Joukowski theorem

Go

Verified Freestream velocity by Kutta-Joukowski theorem

Go

Verified Test section velocity for low speed wind tunnel in terms of height difference of manometric fluid

Go

Verified Test section velocity in low-speed wind tunnel

Go

9 More Fundamentals of Inviscid Incompressible flow Calculators

Go

Verified Current gain of the amplifier in decibels

Go

15 More Gain Calculators

Go

Verified Gearing ratio

Go

Verified Gearing ratio for given hinge moment coefficient

Go

2 More Gearing Ratio Calculators

Go

Created Feed force

Go

Created Radial force

Go

Created Side cutting edge angle for orthogonal cutting

Go

Created Side rake angle for orthogonal cutting

Go

6 More Geometry of Turning Process Calculators

Go

Verified Glide angle for given lift-to-drag ratio

Go

4 More Gliding Flight Calculators

Go

Created Head available at the base of the nozzle

Go

Created Total head at the inlet of pipe for head available at the base of the nozzle

Go

Created Total head available at inlet of pipe for efficiency of power transmission

Go

Verified Hinge moment for given gearing ratio

Go

Verified Hinge moment for given stick force

Go

1 More Hinge Moment Calculators

Go

Verified Energy for blast wave

Go

Verified Radial coordinate of blunt slab blast wave

Go

Verified Simplified pressure ratio for blunt cylinder blast wave

Go

Verified Time required for blast wave

Go

12 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators

Go

Verified Pressure ratio of Blunt-nosed cylinder (first approximation):

Go

Verified Radial coordinate of Blunt-nosed cylinder (first approximation):

Go

Verified Radius for cylinder-wedge body shape

Go

Verified Radius for sphere-cone body shape

Go

5 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators

Go

Verified Mach ratio at high mach number

Go

Verified Pressure ratio for high Mach number

Go

Verified Pressure ratio having high mach number with similarity constant

Go

17 More Hypersonic Flow Calculators

Go

Verified Non-dimensional pressure

Go

Verified Non-dimensional pressure for high mach number

Go

Verified Slenderness ratio with cone radius for hypersonic vehicle

Go

8 More Hypersonic Inviscid Flowfields: Approximate Methods Calculators

Go

Verified Detachment distance of cylinder wedge body shape

Go

Verified Detachment distance of sphere cone body shape

Go

Verified Grid point calculation for shock waves

Go

Verified Nose radius of cylinder-wedge

Go

Verified Nose radius of sphere cone

Go

Verified Pressure ratio for unsteady waves

Go

Verified Ratio of new and old temperature

Go

11 More Hypersonic Inviscid Flowfields: Exact Methods Calculators

Go

Verified Change in velocity for hypersonic flow in x direction

Go

Verified Coefficient of pressure with slenderness ratio and similarity constant

Go

Verified Constant g used for finding the location of perturbed shock

Go

Verified Density ratio with similarity constant having slenderness ratio

Go

Verified Distance from tip of leading edge to base

Go

Verified Non- dimensionalised time

Go

11 More Hypersonic Small-Disturbance Equations Calculators

Go

Verified Boundary-layer momentum thickness using Reynolds number at transition point

Go

Verified Eddy viscosity calculation

Go

Verified Local Mach Number using Reynolds number equation at transition region

Go

Verified Location of transition point

Go

Verified Prandtl number of transition flow

Go

Verified Specific heat at constant pressure for transient flow

Go

Verified Static density at transition point

Go

Verified Static density equation using boundary-layer momentum thickness

Go

Verified Static velocity at transition point

Go

Verified Static velocity using boundary-layer momentum thickness

Go

Verified Static viscosity at transition point

Go

Verified Static viscosity equation using boundary-layer momentum thickness

Go

Verified Transition Reynolds number

Go

3 More Hypersonic Transition Calculators

Go

Verified Large Mach number over flat plate using static temperature and wall temperature

Go

Verified Pressure ratio for cold-wall case the strong interaction

Go

Verified Pressure ratio for cold-wall case the weak interaction

Go

Verified Static density of fluid over flat plate

Go

Verified Static temperature over flat plate using Static Mach Number

Go

Verified Static viscosity using wall temperature and static temperature

Go

Verified viscosity of wall using wall temperature and static temperature

Go

Verified Wall density of fluid over flat plate

Go

Verified Wall temperature over flat plate using Static Mach Number

Go

9 More Hypersonic Viscous Interactions Calculators

Go

Created Dimensions of Rankine half-body

Go

Created Distance between source or sink from origin

Go

Created Distance of stagnation point S from source in flow past a half body

Go

Created Location of stagnation point on x-axis

Go

Created Radial velocity at any radius

Go

Created Radius at any point considering radial velocity

Go

Created Radius of the Rankine circle

Go

Created Stream function at a point

Go

Created Stream function at a point in the combined flow

Go

Created Stream function in sink flow for angle

Go

Created Strength of doublet for stream function

Go

Created Strength of source for radial velocity and at any radius

Go

Created Strength of source for Rankine half body

Go

Created Uniform flow velocity for Rankine half body

Go

Created Uniform flow velocity for stream function at a point in the combined flow

Go

Verified Boundary layer thickness for laminar flow

Go

Verified Moment coefficient about leading-edge for symmetrical airfoil by thin airfoil theory

Go

6 More Incompressible flow over airfoil Calculators

Go

Created Angular velocity considering the depth of parabola

Go

Created Depth of parabola formed at the free surface of water

Go

Created Height or depth of paraboloid for volume of air

Go

Created Rate of flow or discharge

Go

Created Resultant velocity for two velocity components

Go

Created Total pressure force at the bottom of the cylinder

Go

Created Total pressure force on top of cylinder

Go

Verified Newtonian Dynamic pressure

Go

Verified Newtonian pressure distribution over the surface using cosine angle

Go

Verified Nusselt number at stagnation point

Go

Verified Nusselt number for stagnation point on blunt body

Go

Verified Stagnation pressure

Go

2 More Laminar boundary layer at a stagnation point on a blunt body, Calculators

Go

Verified Touchdown velocity

Go

3 More Landing Performance Calculators

Go

Created Length of pipe for difference of pressure in viscous flow

Go

Created Length of pipe for head loss due to friction in viscous flow

Go

Created Length of pipe for loss of pressure head in viscous flow

Go

Created Length of weir considering Bazin's formula with velocity approach

Go

Created Length of weir considering Bazin's formula without velocity approach

Go

Created Length of weir considering Francis's formula

Go

Created Length of weir for broad-crested weir and head of liquid at middle

Go

Created Length of weir for broad-crested weir with velocity approach

Go

Created Length of weir for Discharge over a broad-crested weir

Go

Created Length of weir or notch for velocity of approach

Go

Created Length of weir or notch without velocity of approach

Go

Created Area of the body for lift force in body moving on fluid

Go

Created Length of the cylinder for lift force on a cylinder

Go

Created Lift force for a body moving in a fluid of certain density

Go

Created Lift force on a cylinder for circulation

Go

3 More Lift Force on Body Calculators

Go

Verified Lift-to-drag ratio for given required thrust of aircraft

Go

Verified Thrust of aircraft required for given Lift-to-drag ratio

Go

Verified Weight of aircraft for given Lift-to-drag ratio

Go

Verified Elevator area for given hinge moment coefficient

Go

Verified Elevator Hinge moment coefficient

Go

Verified Elevator Hinge moment for given hinge moment coefficient

Go

2 More Longitudinal Control of Elevator Hinge Moment Calculators

Go

Created Loss of head due to friction

Go

Created Loss of pressure head for viscous flow between two parallel plates

Go

Created Loss of pressure head for viscous flow through circular pipe

Go

Created Head loss due to friction for the efficiency of power transmission

Go

Created Loss of head at entrance of pipe

Go

Created Loss of head at the exit of pipe

Go

Created Loss of head due to bead in pipe

Go

Created Loss of head due to obstruction in pipe

Go

Created Loss of head due to sudden contraction

Go

Created Loss of head due to sudden enlargement at any particular section of pipe

Go

Created Loss of head in equivalent pipe

Go

Verified Load factor for a given pull-down maneuver radius

Go

Verified Load factor for a given pull-up maneuver rate

Go

Verified Pull-down maneuver radius

Go

Verified Pull-up maneuver rate

Go

Verified Velocity for given pull-down maneuver rate

Go

Verified Velocity for given pull-up maneuver radius

Go

Verified Velocity for given pull-up maneuver rate

Go

6 More Maneuvering Flight Calculators

Go

Created Frictional force along tool rake face for given cutting & thrust forces and normal rake angle

Go

21 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators

Go

Verified Coefficient of drag equation with coefficient of normal force

Go

Verified Exact normal shock wave maximum coefficient of pressure

Go

Verified Force exerted on surface in terms of static pressure

Go

Verified Mass flux incident on a surface area

Go

Verified Maximum Pressure coefficient

Go

9 More Newtonian Flow Calculators

Go

Verified Density behind normal shock for given upstream density and Mach number

Go

Verified Static pressure behind normal shock for given upstream pressure and Mach number

Go

Verified Static temperature behind normal shock for given upstream temperature and Mach number

Go

Verified Temperature ratio across a normal shock

Go

16 More Normal Shock Waves Calculators

Go

Created Head of liquid above the V-notch

Go

Created Head of liquid over the crest

Go

Created Length of crest of the weir or notch

Go

Created Length of section for discharge over rectangle notch or weir

Go

Created Time required to empty a reservoir

Go

Created Time required to empty a tank with a triangular weir or notch

Go

Verified Component of downstream Mach number normal to oblique shock for given normal upstream Mach number

Go

Verified Density behind oblique shock for given upstream density and normal upstream Mach number

Go

Verified Density ratio across the oblique shock

Go

Verified Forward Mach angle of expansion fan

Go

Verified Pressure behind oblique shock for given upstream pressure and normal upstream Mach number

Go

Verified Pressure ratio across the expansion fan

Go

Verified Pressure ratio across the oblique shock

Go

Verified Temperature behind oblique shock for given upstream temperature and normal upstream Mach number

Go

Verified Temperature ratio across the expansion fan

Go

Verified Temperature ratio across the oblique shock

Go

9 More Oblique Shock and Expansion Waves Calculators

Go

Verified Parallel upstream flow components after shock as Mach tends to infinite

Go

Verified Perpendicular upstream flow components behind the shock wave

Go

13 More oblique shock relation Calculators

Go

Created Absolute pressure head at constant head and atmospheric pressure head

Go

Created Area at vena contracta for discharge and constant head

Go

Created Area of mouthpiece In Borda's mouthpiece running free

Go

Created Area of mouthpiece In Borda's mouthpiece running full

Go

Created Area of orifice considering time of emptying a hemispherical tank

Go

Created Area of tank while considering time for emptying a tank

Go

Created Atmospheric pressure head at constant head and absolute pressure head

Go

Created Coefficient of Contraction given Area of Orifice

Go

Created Head of liquid for head loss and coefficient of velocity

Go

Created Head of the liquid above the centre of orifice

Go

Created Horizontal distance for coefficient of velocity and vertical distance

Go

Created Loss of head due to fluid resistance

Go

Created Loss of head due to sudden enlargement

Go

Created Theoretical velocity

Go

Created Velocity of liquid at C-C for Hc, Ha, and H

Go

Created Vertical distance for coefficient of velocity and horizontal distance

Go

Verified Area of composite wall of 2 layers

Go

Verified Area of composite wall of 3 layers

Go

Verified Inner surface temperature of a composite wall of 2 layers in series

Go

Verified Inner surface temperature of a composite wall of 3 layers in series

Go

Verified Inner surface temperature of a plane wall

Go

Verified Length of 3rd layer of composite wall for a given temperature difference

Go

Verified Temperature at distance x from the inner surface in the wall

Go

Verified Thermal resistance of a composite wall with 2 layers in series

Go

Verified Thermal resistance of a composite wall with 3 layers in series

Go

Verified Thermal Resistance of a wall

Go

12 More Plane walls Calculators

Go

Created Power absorbed in collar bearing

Go

Created Power absorbed in foot-step bearing

Go

Created Power absorbed in overcoming viscous resistance in journal bearing

Go

Verified Power available for reciprocating engine-propeller combination

Go

Verified Propeller efficiency for reciprocating engine-propeller combination

Go

1 More Power Available and Maximum Velocity Calculators

Go

Verified Power required for given total drag force

Go

Verified Total drag force for given required power

Go

8 More Power Required for Level Unaccelerated Flight Calculators

Go

Created Efficiency of power transmission in flow through pipes

Go

Created Efficiency of power transmission through nozzle for velocity and total head

Go

Created Efficiency of power transmission through the nozzle

Go

Verified Dynamic pressure in incompressible flow

Go

Verified Pressure difference measured by manometer in low-speed wind tunnel

Go

Verified Total pressure in incompressible flow

Go

10 More Pressure Calculators

Go

Verified Radial velocity for 2-D incompressible source flow

Go

2 More Radial Velocity Calculators

Go

Verified Endurance of Propeller-Driven Airplane

Go

Verified Propeller Efficiency for given Endurance of Propeller-Driven Airplane

Go

Verified Propeller Efficiency for given Range and lift-to-drag ratio of Propeller-Driven Airplane

Go

Verified Propeller Efficiency for given Range of Propeller-Driven Airplane

Go

Verified Range of Propeller-Driven Airplane

Go

Verified Range of Propeller-Driven Airplane for given lift-to-drag ratio

Go

Verified Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane

Go

Verified Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane

Go

Verified Specific Fuel Consumption for given Range of Propeller-Driven Airplane

Go

1 More Range and Endurance of Propeller-Driven Airplane Calculators

Go

Verified Thrust available for given excess power

Go

9 More Rate of Climb Calculators

Go

Verified Chord length for flat plate case

Go

Verified Local Reynolds number

Go

Verified Mach number at reference temperature

Go

Verified Overall skin-friction drag coefficient for incompressible flow

Go

Verified Reference temperature equation

Go

Verified Stanton Number obtained from classical theory

Go

Verified Static viscosity of plate using chord length for flat plate case

Go

Verified Wall temperature using reference temperature

Go

7 More Reference Temperature Method Calculators

Go

Verified Aircraft forward velocity for given normal component of side velocity

Go

Verified Aircraft sideslip velocity for given dihedral angle

Go

Verified Dihedral angle for given sideslip velocity

Go

Verified Normal component of aircraft side velocity for given dihedral angle

Go

Verified Normal component of aircraft side velocity for given forward velocity

Go

Created Rotational speed considering power absorbed and torque in journal bearing

Go

Created Rotational speed for torque required in collar bearing

Go

Created Rotational speed for torque required in foot-step bearing

Go

Verified Coefficient of pressure equation using specific heat ratio

Go

Verified curvilinear grid location equation

Go

Verified Density equation using enthalpy and pressure

Go

Verified Enthalpy equation using pressure and density

Go

Verified pressure equation using Enthalpy and density

Go

6 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators

Go

Verified Convection resistance for a spherical layer

Go

Verified Heat flow rate through spherical composite wall of 2 layers in series

Go

Verified Inner surface temperature of a spherical wall

Go

Verified Outer surface temperature of a spherical wall

Go

Verified Thermal resistance of a spherical composite wall of 2 layers in series with convection

Go

Verified Thickness of the spherical wall to maintain given temperature difference

Go

Verified Total thermal resistance of a spherical wall of 2 layers without convection

Go

Verified Total thermal resistance of a spherical wall of 3 layers without convection

Go

Verified Total thermal resistance of a spherical wall with convection on either side

Go

2 More Spheres Calculators

Go

Created Stagnation density considering other stagnation properties of the fluid

Go

Created Stagnation density considering the compressible fluid flow

Go

Created Location of stagnation points for a rotating cylinder in a uniform flow field

Go

Created Radius of cylinder for lift coefficient in a rotating cylinder with circulation

Go

Created Radius of the cylinder for a single stagnation point

Go

Created Radius of the cylinder for location of stagnation points

Go

Created Stagnation pressure considering other stagnation properties of the fluid

Go

Created Stagnation pressure for the compressible fluid flow

Go

Created Stagnation temperature considering other stagnation properties of the fluid

Go

Created Stagnation temperature considering the compressible fluid flow

Go

Verified Elevator area for given stick force

Go

Verified Flight velocity for given stick force

Go

Verified Stick length for given stick force

Go

4 More Stick Forces Calculators

Go

Verified Stream function for 2-D Doublet flow

Go

Verified Stream function for 2-D Vortex flow

Go

Verified Stream function for lifting flow over a circular cylinder

Go

Verified Stream function for semi-infinite body

Go

Verified Stream function for uniform incompressible flow

Go

4 More Stream Function Calculators

Go

Verified Angle of incidence of tail

Go

Verified Lift due to tail only

Go

Verified Lift due to wing only

Go

Verified Tail area for given tail efficiency

Go

Verified Tail Efficiency for given lift coefficients

Go

Verified Tail lift coefficient for given pitching moment

Go

Verified Tail Lift Coefficient of wing-tail combination

Go

Verified Tail lift for given tail pitching moment

Go

Verified Tail Pitching moment coefficient

Go

Verified Tail Pitching moment for given lift coefficient

Go

Verified Total Lift of wing-tail combination

Go

Verified Wing Lift Coefficient of wing-tail combination

Go

9 More Tail Contribution Calculators

Go

Verified Tail area for given tail moment coefficient

Go

Verified Tail Efficiency for given pitching moment coefficient

Go

Verified Tail lift coefficient for given pitching moment coefficient

Go

Verified Tail moment arm for given tail moment coefficient

Go

Verified Tail Pitching moment coefficient for given tail efficiency

Go

9 More Tail Contribution Contd Calculators

Go

Verified Liftoff velocity for given weight

Go

13 More Takeoff Performance Calculators

Go

Verified Tangential velocity for non-lifting flow over circular cylinder

Go

2 More Tangential Velocity Calculators

Go

Created Thickness of oil film for shear force in journal bearing

Go

Created Thickness of oil film for speed and diameter of shaft in journal bearing

Go

Created Thickness of oil film for torque required in foot-step bearing

Go

Created Thrust force for given cutting force, shear angle & force along the shear force

Go

Created Thrust force for given cutting force, shear angle & force normal to shear force

Go

2 More Thrust Force Calculators

Go

Verified Coefficient of Lift for given thrust and weight

Go

Verified Lift coefficient for given minimum required thrust

Go

Verified Minimum Thrust required for given lift coefficient

Go

Verified Thrust for given coefficients of lift and drag

Go

Verified Weight of aircraft for given coefficients of lift and drag

Go

7 More Thrust Required for Level Unaccelerated Flight Calculators

Go

Created Time of emptying a circular horizontal tank

Go

Created Time of emptying a hemispherical tank

Go

Created Time of emptying a tank through an orifice at bottom

Go

Created Torque required considering power absorbed in journal bearing

Go

Created Torque required to overcome the shear force in journal bearing

Go

Created Torque required to overcome viscous resistance in collar bearing

Go

Created Torque required to overcome viscous resistance in foot-step bearing

Go

Created Total torque measured by strain in rotating cylinder method

Go

Created Average height of irregularities for turbulent flow in pipes

Go

Created Discharge through pipe for power required and head loss in turbulent flow

Go

Created Head loss due to friction for power required and discharge in turbulent flow

Go

Created Power required to maintain the turbulent flow

Go

Created Roughness Reynold number for turbulent flow in pipes

Go

Created Shear stress developed for turbulent flow in pipes

Go

Created Shear velocity for turbulent flow in pipes

Go

11 More Turbulent flow Calculators

Go

Created Angular speed of outer cylinder in rotating cylinder method

Go

Created Maximum velocity at any radius with a velocity, and radius of pipe

Go

Created Velocity at any radius, radius of pipe, and maximum velocity

Go

Created Velocity of piston or body for movement of piston in dash-pot

Go

Created Velocity of sphere in falling sphere resistance method

Go

Created Freestream velocity for a single stagnation point

Go

Created Freestream velocity for lift coefficient in a rotating cylinder with circulation

Go

Created Freestream velocity for lift coefficient with tangential speed

Go

Created Tangential velocity for single stagnation point

Go

Created Tangential velocity of the cylinder with the lift coefficient

Go

Created Velocity of airfoil for circulation developed on the airfoil

Go

Created Velocity at section 1-1 for sudden enlargement

Go

Created Velocity at section 2-2 for sudden contraction

Go

Created Velocity at section 2-2 for sudden enlargement

Go

Created Velocity at the outlet for head loss at the exit of pipe

Go

Created Velocity of flow at the outlet of the nozzle

Go

Created Velocity of flow at the outlet of the nozzle for efficiency and head

Go

Created Velocity of fluid for head loss due to obstruction in a pipe

Go

Created Velocity of fluid in pipe for head loss at the entrance of a pipe

Go

Created Velocity of liquid at vena-contracta

Go

Created Velocity of sound wave considering Mach angle in the compressible fluid flow

Go

Created Velocity of sound wave in Mach number for the compressible fluid flow

Go

Created Velocity of sound wave in terms of an adiabatic process

Go

Created Velocity of sound wave in terms of bulk modulus

Go

Created Velocity of sound wave in terms of isothermal process

Go

Created Viscosity of fluid or oil for capillary tube method

Go

Created Viscosity of fluid or oil for movement of piston in dash-pot

Go

Created Viscosity of fluid or oil in falling sphere resistance method

Go

Created Viscosity of fluid or oil in rotating cylinder method

Go

1 More Viscosity of Fluid Calculators

Go

Created Buoyant force in falling sphere resistance method

Go

Created Density of fluid in falling sphere resistance method

Go

Created Diameter of capillary tube

Go

Created Diameter of shaft for speed and shear stress of fluid in journal bearing

Go

Created Diameter of sphere in falling sphere resistance method

Go

Created Difference of pressure for viscous flow between two parallel plates

Go

Created Difference of pressure for viscous or laminar flow

Go

Created Discharge in capillary tube method

Go

Created Drag force in falling sphere resistance method

Go

Created External or outer radius of collar for total torque

Go

Created Internal or inner radius of collar for total torque

Go

Created Length for difference of pressure in viscous flow between two parallel plates

Go

Created Length for pressure head loss in viscous flow between two parallel plates

Go

Created Length of tube in capillary tube method

Go

Created Radius of pipe from maximum velocity and velocity at any radius

Go

Created Radius of shaft for torque required in foot-step bearing

Go

Created Shear force for torque and diameter of shaft in journal bearing

Go

Created Shear force or viscous resistance in journal bearing

Go

Created Shear stress in the fluid or oil of journal bearing

Go

Created Speed of rotation for shear force in journal bearing

Go

Verified Aerodynamic heating to surface

Go

Verified Chapman–Rubesin factor

Go

Verified Coefficient of friction using Stanton equation for incompressible flow

Go

Verified Density calculation using Chapman–Rubesin factor

Go

Verified Stanton number for incompressible flow

Go

Verified Static Density calculation using Chapman–Rubesin factor

Go

Verified Static viscosity calculation using Chapman–Rubesin factor

Go

Verified Thermal conductivity using Prandtl number

Go

Verified Viscosity calculation using Chapman–Rubesin factor

Go

7 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating Calculators

Go

List of Calculators by Maiarutselvan V