Table of Flow Properties -- For a Normal Shock Property :

Input flow variable:

1. M1 ( > 1 )2. P2/P1
3. 4. T2/T1
5. Pt2/Pt1(=A1*/A2*)6. Pt2/P1 ( > 1.893 )
7. M2 ( < 1 )
:
Choose your case:
And it's value is:

Output Flow Properties:

M1
P2/P1
T2/T1
Pt2/Pt1
Pt2/P1
M2

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