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Oblique Shock Prandtl Meyer: OBLIQUE SHOCK M7.0

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 M7.08 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 M7.050.399656.1061451.4743.254656.977762.2339588.869811.825
OBLIQUE SHOCK M7.0100.406715.23445101.4743.254656.908564.3806587.707916.3818
OBLIQUE SHOCK M7.0150.419144.40282151.4743.254656.784197.5791286.477421.5983
OBLIQUE SHOCK M7.0200.438133.66295201.4743.254656.5880411.8399285.130327.2767
OBLIQUE SHOCK M7.0250.465853.02625251.4743.254656.2883917.1071983.594133.3462
OBLIQUE SHOCK M7.0300.506542.47658301.4743.254655.82123.309681.743239.8538
OBLIQUE SHOCK M7.0350.569811.98538351.4743.254655.0329530.4329779.309947.0225
OBLIQUE SHOCK M7.0400.687391.50317401.4743.254653.3899538.8226975.445855.6748

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