Compressible Flow Calculator
Need to perform a simple side calculation? Try the
Quick Calculator
Isentropic Flow Relations
INPUT:
Mach number
T/T0
p/p0
rho/rho0
A/A* (sub)
A/A* (sup)
Mach angle (deg)
P-M angle (deg)
=
Gamma =
(perfect gas)
(all angles in degrees)
Mach number =
Mach angle =
A/A* =
P-M angle =
p/p
0
=
p/p* =
rho/rho
0
=
rho/rho* =
T/T
0
=
T/T* =
Normal Shock Relations
INPUT:
M1
M2
p2/p1
rho2/rho1
T2/T1
p02/p01
p1/p02
=
Gamma =
(perfect gas)
M
1
=
M
2
=
p
02
/p
01
=
p
1
/p
02
=
p
2
/p
1
=
rho
2
/rho
1
=
T
2
/T
1
=
Oblique Shock Relations
INPUT:
M
1
=
Turn angle (weak)
Turn angle (strong)
Wave angle
M1n
=
Gamma =
(perfect gas)
(all angles in degrees)
M
1
=
M
2
=
Turn angle =
Wave angle =
p
2
/p
1
=
p
02
/p
01
=
rho
2
/rho
1
=
T
2
/T
1
=
M
1n
=
M
2n
=
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