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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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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Question Posted: Apr 29, 2024 06:01 AM

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At low speed Incompressible flow, the pressure coefficient at a given point on the wing is 0.54.

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Aerodynamics

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