Show that for an heaving-plunging airfoil the aerodynamic propulsion efficiency is (eta=frac{F^{2}+G^{2}}{F}).
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Show that for an heaving-plunging airfoil the aerodynamic propulsion efficiency is \(\eta=\frac{F^{2}+G^{2}}{F}\).
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Related Book For 
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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