Isentropic Flow Calculations

• Calculate Continuity Equation for Incompressible Flow

• Calculate Continuity Equation for Compressible Flow

• Calculate Bernoulli's Equation

• Calculate Pressure at Exit of Convergent Duct

• Isentropic Flow Calculations

• Calculate Velocity at Throat of Supersonic Wind Tunnel

• Calculate Velocity at Exit of Supersonic Wind Tunnel

• Calculate Area at Throat and Exit of Supersonic Wind Tunnel

• Calculate Velocity at Exit

• Calculate Local Shear Stress in Laminar Flow Direction

• Calculate Local Shear Stress in Turbulent Flow Direction

• Calculate Airflow Velocity in Test Section of Subsonic Wind Tunnel

• Calculate True Velocity of an Airplane

• Calculate Equivalent Airspeed of an Airplane

• Calculate Reservoir Pressure for Supersonic Wind Tunnel

• Calculate Temperature Area Ratio for Supersonic Wind Tunnel

• Calculate Pressure at Stagnation Point

• Calculate Temperature at Stagnation Point

• Calculate Density at Stagnation Point

• Calculate Mass Flow through the Nozzle

• Calculate Velocity at a point on an Airfoil

• Calculate Mach Number

• Calculate Mach Number of Flow at Nozzle

• Calculate Mach Number of Flow at Exit

• Calculate True Airspeed

• Calculate Calibrated Airspeed

• Calculate Pressure Measured by Pitot Tube

• Calculate Boundary Layer Thickness at Trailing Edge

• Calculate Drag force on Plate

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Calculate Isentropic Flow Parameters

For calculating the isentropic flow parameters we consider that the airplane is flying at standard sea-level conditions.

In order to calculate the pressure at a point using the isentropic flow relation we need to input the

The temperature at a point on the wing in Kelvin K.

Performing the calculation gives us the pressure P2 value at a point on the wing.

If we have the density value instead of the temperature value at a point on the wing then we can also calculate the pressure at a point using the isentropic flow relation. After calculation, it gives at pressure P2 at a point on the wing.

Download Free Program to Calculate the Isentropic Flow Relations