The tapered symmetric thin wing geometry is shown in Fig. 4.8. If this wing under goes a
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The tapered symmetric thin wing geometry is shown in Fig. 4.8. If this wing under goes a simple harmonic motion in vertical direction, find the amplitude of sectional lift coefficients in terms of the amplitude of the motion.
Fig. 4.8
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Related Book For 
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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