[alireza.nasa]

dear friends

i'm simulating hypersonic flow condition around cone.

hew i should import my wind tunnel condition in fluent

test section condition :
mach :5.1
stagnation pressure=10 Mpa
stagnation temperature : 630 K
dynamic pressure : 30.6
reynolds : 0.847*10e7

i want to have :

static pressure:?

static temperature:?

density :?

is it right to derive this parameters from super sonic tables?? dose it mean the stagnation pressure = Po reservoir ??