Find and plot the lift response of the airfoil at Mach number of (sqrt{2}) experiencing the gust
Question:
Find and plot the lift response of the airfoil at Mach number of \(\sqrt{2}\) experiencing the gust described in 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
Step by Step Answer:
Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
Question Posted: