Derive Eq. 8.37 for the thrust coefficient of an airfoil in pure pitching about the point (a)

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Derive Eq. 8.37 for the thrust coefficient of an airfoil in pure pitching about the point $a$ with reduced frequency $k$.

Eq. 8.37

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Fundamentals Of Modern Unsteady Aerodynamics

ISBN: 9783030607760,9783030607777

3rd Edition

Authors: Ülgen Gülçat

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Question Posted: Apr 17, 2024 04:06 AM

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Derive Eq. 8.37 for the thrust coefficient of an airfoil in pure pitching about the point (a)

Question:

de tan (- h+da (1) cos(x(t))) + (1) U da(t) sin(x(t))'

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Fundamentals Of Modern Unsteady Aerodynamics

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