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REPORT 1135 - NASA

REPORT 1135 . equations , TABLES, AND CHARTS FOR. COMPRESSIBLE FLOW. By AMES RESEARCH STAFF. Ames Aeronautical Laboratory Moffett Field, Calif. REPORT 1135 . equations , TABLES, AND CHARTS FOR COMPRESSIBLE FLOW 1. By AMEs RESEARCH STAFF. SUMMARY normal force C_ normal-force coefficient for cones, q_S_. This REPORT , which is a revision and extension of NACA TN C_, specific heat at constant pressure 1_28, presents a compilation of equations , tables, and charts Ce specific heat at constant volume useful in the analysis of high-speed flow of a compressible fluid. h enthalpy per unit mass, u-_pv The equations provide relations for continuous o_e-dimensional l characteristic reference length flow, normal and oblique shock waves, and Prandtl-Meyer M Mach number, V.

BERNOULLI*SEQUATION Combination of equations (32b) and (35) gives Bernoulli's equation for compressible flow in the form "y--1 3" Pt P _,' = 3" Pt [isen, perf] (36) RELATIONSBETWEEN LOCALANDFREE-STREAMCONDITIONS With the aid of the foregoing equations it can be shown that T , _--1 M: V 2

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