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)
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)
Spencer, Nelson W.
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Other Identifiers: UMR4456
Subject(s): Pressure -- Measurement.
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