At low speed Incompressible flow, the pressure coefficient at a given point on the wing is 0.54.
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At low speed Incompressible flow, the pressure coefficient at a given point on the wing is 0.54. When the free flow Mach number is 0.58, by use of
(1) Prandtl-Glauert law
(2) Karman-Qian law
(3) Laitone law.
What is the pressure coefficient?
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