For a chordwise flexible airfoil obtain the quasi unsteady edge velocity, Eq. 8.41, and the suction force
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For a chordwise flexible airfoil obtain the quasi unsteady edge velocity, Eq. 8.41, and the suction force coefficient, Eq. 8.42, formulae assuming that the parabolic camber of the airfoil, whose maximum camber is at the midchord, changes simple harmonically.
Eq. 8.41
Eq. 8.42
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Related Book For 
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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