Created by: Dr. K. N. Ghia Scott E. Will Modified by: Marshall C Galbraith Last updated: July 17, 2002
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Isentropic Flow Relations Perfect Gas, Gamma = , angles in degrees.
INPUT: Mach number T/T0 p/p0 rho/rho0 A/A* (sub) A/A* (sup) Mach angle (deg.) P-M angle (deg.) =
Mach angle=
p/po=
r/ro=
T/To=
p/p*=
r/r*=
T/T*=
Normal Shock Relations Perfect Gas, Gamma =
INPUT: M1 M2 p2/p1 rho2/rho1 T2/T1 p02/p01 p1/p02 =
Oblique Shock Relations Perfect Gas, Gamma = , angles in degrees.
INPUT: M1 = Turn angle (weak shock) Turn angle (strong shock) Wave angle M1n =
Adapted from Javascript by William J. Devenport, Department of Aerospace and Ocean Engineering, Virginia Tech.
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