The wing-tail interaction problem for \(\mathrm{k}=0.75\) and \(\mathrm{M}=0\) is shown in Fig. P5.15.

For the simple harmonic plunging obtain the lift amplitude. Take 10 panels in spanwise direction with Multhopp distribution and 5 panels in chordwise direction. The distance between the wing and the tail at the root is \(0.6 \mathrm{x} / \mathrm{l}\).

Fig. P5.15

Transcribed Image Text:

y/l 1 A 1 2 3 x/1 4