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1.4 is plotted air tables Ref Based on constant Btu per lb calculations computed from Equation conservation of energy conservation of mass considered constant CONSTANT Report degree Rankine density downstream values energy equation enthalpy Equation 15 error flow Mach Number flow relations ft lb ft per sec heat ratio determination heats of air high Mach Numbers iiii Iiiii iiiliii Isentropic Flow lb mass lb per degree lb per slug liiiiiiiiiii Mach Numbers greater MICHIGAN Page MICHIGAN Report Normal Shock Wave Number are plotted Number of six Number on Figure plotted on Figures plotted versus Mach Position immediately upstream SHOCK FLOW specific heat ratio ssss ssssssssssss stagnation pressure stagnation temperature Stagnation value Stream temperature temperature of 393°R temperature of 520°R UMM-6 Figure UMM-6 UNIVERSITY undisturbed flow temperature UNIVERSITY OF MICHIGAN upstream conditions iu upstream Mach Number upstream static temperature VARIATION versus Mach Number zero intensity