11. Hypersonic Aerodynamics
W.H. Mason Hypersonic Aerodynamics 11-7 7/31/16 Figure 11-6. Sketch defining the hypersonic directional stability problem Now, for a high-speed flow, we will assume that the vertical tail is a two-dimensional surface with a constant pressure on each side, so that . We will consider two cases, one supersonic, the other hypersonic.
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