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Temperature rise across the normal shock
Directly from the equation of state and Eqns (6.43) and (6.45):
Tl — El I El
Ti ~Pi/ Pi
Tj = (2^M – (7- 1) (2 + (7- 1)M(
Ti 7+1 Д (7+1 )M )
For air
T2 1M – 5/M} + 34 Ti ~ 36
Since the flow is non-heat conducting the total (or stagnation) temperature remains constant.
