1. Consider an infinitely thin, fiat plate. Using Newtonian theory, show that CL.1Dv. = 0.77 and that it occurs at a = 54.7°. 2. Consider hypersonic flow over an infinitely thin, fiat plate. The zero-lift drag coefficient is denoted by Consider that the wave drag coefficient is given by the Newtonian result for drag coefficient-that is, by Eq. (10.12). Also assume that the lift coefficient is given by the Newtonian result in Eq. (10.11). We wish to examine some results associated with (IJ D)”””’ for this fiat plate. Because (LID) …. , occurs at a small angle of attack, make the assumption of small a in . (10.11) and (10.12). Under these conditions, show that at maximum and occurs at a = C~~; and (b) the wave drag coefficient
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