For Mach number 0.7, find the lift response of the airfoil subjected to the gust given by
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For Mach number 0.7, find the lift response of the airfoil subjected to the gust given by Problem 3.13.
Problem 3.13
If the gust intensity with time varies as given in Fig. 3.16, obtain the lift and the moment coefficient changes about the midchord and their plots with respect to time.
Fig. 3.16
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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