At a given point on the surface of the wing, the flow velocity is 130 m/s. Calculate the pressure coefficient at this point
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At a given point on the surface of the wing of the airplane in Problem 3.6, the flow velocity is 130 m/s. Calculate the pressure coefficient ...
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Answer:
This question is not complete ,because to find pressure coefficient you need free stream velocity(v∞) also, but here only V is given.
So the complete question is :
A Pitot tube on an airplane flying at standard sea level reads 1.07 x 105N/m2.
What is the velocity of the airplane? At a given point on the surface of the
wing of the airplane the flow velocity is 130 m/s. Calculate the pressure
coefficient at this point.
Solution:
Explanation:
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