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Oblique Shock Prandtl Meyer: OBLIQUE SHOCK M8.0

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 M8.08 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 M8.050.395136.8646351.4843.790874.472472.4771388.899810.846
OBLIQUE SHOCK M8.0100.402045.76232101.4843.790874.386865.1848287.769115.5284
OBLIQUE SHOCK M8.0150.414184.74778151.4843.790874.23329.3012686.57320.8605
OBLIQUE SHOCK M8.0200.432693.88661201.4843.790873.9913514.8226685.265626.6187
OBLIQUE SHOCK M8.0250.459633.17515251.4843.790873.623221.6619583.778932.7307
OBLIQUE SHOCK M8.0300.498982.58022301.4843.790873.0524329.7127381.996339.2415
OBLIQUE SHOCK M8.0350.55952.06241351.4843.790872.1016838.9312679.675646.3546
OBLIQUE SHOCK M8.0400.66841.56976401.4843.790870.1889549.6513676.096654.7684

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