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Oblique Shock Prandtl Meyer: OBLIQUE SHOCK M10.0

5 to 40

Oblique shock wave angles and Prandtl-Meyer expansion function for supersonic and hypersonic flow. Covers two record types: (1) PRANDTL_MEYER — nu(M) expansion angle and Mach angle mu(M) for Mach 1.0–10.0; (2) OBLIQUE_SHOCK — weak and strong shock angles, downstream Mach number, and pressure ratio for each (M1, deflection angle) combination, Mach 1.0–10.0, deflection angles 5–40 degrees. gamma=1.4 throughout.

Mechanical Engineeringflow type: OBLIQUE SHOCK M10.08 rows
flow typesort key numM2 strong (dimensionless)M2 weak (dimensionless)deflection angle deg (deg)gamma (dimensionless)mach number (dimensionless)max deflection angle deg (deg)p2 over p1 strong (dimensionless)p2 over p1 weak (dimensionless)strong shock angle deg (deg)weak shock angle deg (deg)
OBLIQUE SHOCK M10.050.389768.286151.41044.429116.459673.0242388.93479.5193
OBLIQUE SHOCK M10.0100.396486.65726101.41044.429116.334337.0748987.840414.4266
OBLIQUE SHOCK M10.0150.408295.27926151.41044.429116.1096713.4043786.68419.9416
OBLIQUE SHOCK M10.0200.426264.20738201.41044.429115.7569321.9614485.422525.8178
OBLIQUE SHOCK M10.0250.452323.3782251.41044.429115.2220832.5824283.992431.9931
OBLIQUE SHOCK M10.0300.490152.71653301.41044.429114.398545.0785282.286938.5171
OBLIQUE SHOCK M10.0350.547662.16073351.41044.429113.0446659.3412180.090345.5769
OBLIQUE SHOCK M10.0400.647871.65102401.41044.429110.4172475.7237376.800853.7582

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