APPENDIX C Normal Shock Table

Normal shock relations that are used in calculating the jump conditions, for a calorically perfect gas (i.e., γ = constant), are summarized below:

(C.1)numbered Display Equation
(C.2)numbered Display Equation
(C.3)numbered Display Equation
(C.4)numbered Display Equation
(C.5)numbered Display Equation
(C.6)numbered Display Equation
(C.7)numbered Display Equation

We have derived these expressions in Chapter 2.

Normal Shock Table γ = 1.4

M1 M2 T2/T1 p2/p1 / pt2/pt1 pt2/p1 /
1 1 1 1 1 1 1.8929 0
1.02 0.9805 1.0132E+00 1.0471 ...

Get Aircraft Propulsion, 2nd Edition now with the O’Reilly learning platform.

O’Reilly members experience books, live events, courses curated by job role, and more from O’Reilly and nearly 200 top publishers.