Table of pressure ratios P[subscript i]/P[subscript c] and P[subscript c]/P[subscript a] vs. mach number for a 150 right circular supersonic cone (¿=1.405)
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Table of pressure ratios P[subscript i]/P[subscript c] and P[subscript c]/P[subscript a] vs. mach number for a 150 right circular supersonic cone (¿=1.405)