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Calculate Velocity at a Point on Wing and Airfoil Method to Calculate the Velocity at a Point on the Airfoil |
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Aerospace
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How to Calculate the Velocity at a point on the Airfoil In this article we would look into how to calculate the velocity at a point on the airfoil considering compressible flow. |
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In order to calculate the velocity, we need to have,
The freestream Pressure P(inf) in lb/ft^2 The freestream Velocity V(inf) in mi/hr The freestream Density row(inf) in slug/ft^3 The pressure at a point on the airfoil Pa in lb/ft^2
For air, we know that Cp = 6006 ft.lb/slug.R
Performing the calculation, we get the freestream temperature, the temperature at point A on the airfoil Ta and the Velocity at the point A on the Airfoil.
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Download Free Program to Calculate the Velocity at a Point on an Airfoil
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