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

image text in transcribed

Step by Step Answer:

Question Posted: