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An air stream of Mach number 1 = 2.25 and static pressure 1 = 125 first undergoes expansion around a = 27 corner followed by
An air stream of Mach number 1 = 2.25 and static pressure 1 = 125 first undergoes expansion around a = 27 corner followed by a compression corner of the same angle
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Understanding Business Ethics
Authors: Peter A. Stanwick, Sarah D. Stanwick
3rd Edition
9781506303239
