Obtain the time dependent but steady lift coefficient, Eq. 8.48, and the boundary layer edge velocity, Eq.
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Obtain the time dependent but steady lift coefficient, Eq. 8.48, and the boundary layer edge velocity, Eq. 8.49 for a chordwise flexible parabolically cambered thin airfoil whose equation is given by Eq. 8.46 and maximum camber location along the chord is given by \(p\).
Eq. 8.48
Eq. 8.49
Eq. 8.46
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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