Oblique Shock Prandtl Meyer
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.
Attributes
mach_numberdimensionless
deflection_angle_degdeg
weak_shock_angle_degdeg
strong_shock_angle_degdeg
M2_weakdimensionless
M2_strongdimensionless
p2_over_p1_weakdimensionless
p2_over_p1_strongdimensionless
max_deflection_angle_degdeg
nu_degdeg
mu_degdeg
gammadimensionless
Browse data
PRANDTL_MEYER3 rowsOBLIQUE_SHOCK_M1.31 rowOBLIQUE_SHOCK_M1.41 rowOBLIQUE_SHOCK_M1.52 rowsOBLIQUE_SHOCK_M1.62 rowsOBLIQUE_SHOCK_M1.73 rowsOBLIQUE_SHOCK_M1.83 rowsOBLIQUE_SHOCK_M1.93 rowsOBLIQUE_SHOCK_M2.03 rowsOBLIQUE_SHOCK_M2.13 rowsOBLIQUE_SHOCK_M2.23 rowsOBLIQUE_SHOCK_M2.33 rowsOBLIQUE_SHOCK_M2.43 rowsOBLIQUE_SHOCK_M2.53 rowsOBLIQUE_SHOCK_M2.63 rowsOBLIQUE_SHOCK_M2.73 rowsOBLIQUE_SHOCK_M2.83 rowsOBLIQUE_SHOCK_M2.93 rowsOBLIQUE_SHOCK_M3.03 rowsOBLIQUE_SHOCK_M3.253 rowsOBLIQUE_SHOCK_M3.53 rowsOBLIQUE_SHOCK_M3.753 rowsOBLIQUE_SHOCK_M4.03 rowsOBLIQUE_SHOCK_M4.253 rowsOBLIQUE_SHOCK_M4.53 rowsOBLIQUE_SHOCK_M4.753 rowsOBLIQUE_SHOCK_M5.03 rows
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