Consider a flat plate at an angle of attack in an inviscid supersonic flow. From linear theory,

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Consider a flat plate at an angle of attack in an inviscid supersonic flow. From linear theory, what is the value of the maximum lift-to-drag ratio, and at what angle of attack does it occur?

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Fundamentals Of Aerodynamics

ISBN: 9781259129919

6th Edition

Authors: John Anderson

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Question Posted: Aug 05, 2022 12:14 AM

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Consider a flat plate at an angle of attack in an inviscid supersonic flow. From linear theory,

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Solution From the linear theory the maximum lifttodrag ratio occurs at ...View the full answer

Fundamentals Of Aerodynamics

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