An airplane wing of 2 m chord length (leading edge to trailing edge distance) and 11 m

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An airplane wing of 2 m chord length (leading edge to trailing edge distance) and 11 m span flies at 200 km/hr in air at 30°C. Assume that the drag force of the wing surfaces is like that of a flat plate.

a. What is the friction drag on the wing?

b. What power is required to overcome this?

c. How much of the chord has laminar flow?

d. What will be the change in drag if a turbulent boundary layer is tripped at the leading edge?

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Engineering Fluid Mechanics

ISBN: 9781118880685

11th Edition

Authors: Donald F. Elger, Barbara A. LeBret, Clayton T. Crowe, John A. Robertson

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Question Posted: Jun 22, 2021 05:49 AM

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An airplane wing of 2 m chord length (leading edge to trailing edge distance) and 11 m

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a To calculate the friction drag on the wing we need to know the air density the dynamic viscosity o...View the full answer

Engineering Fluid Mechanics

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