Derive Eq. 8.37 for the thrust coefficient of an airfoil in pure pitching about the point (a)
Question:
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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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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