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Problem 2 (20 points) Consider a subsonic compressible flow in cartesian coordinates (x and y in meters), with velocity poten
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Tables

Concu 513 Springer Science+Business Media Dordrecht 2015 R. Vos and S. Farokhi, Introduction to Transonic Aerodynamics, FluidAppendix A: Isentropic Flow Table 517 T/T* Table A.1 (continued) M T/T PI/P 2.82 2.59E+00 2.80E+01 2.84 2.61E+00 2.88E+01 2.8

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