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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. expansions for both perfect and imperfect gases. The tables a present useful dimensionless ratios for continuous one-dimen- pressure 2. P. sional flow and for normal shock waves as functions of Mach dynamic pressure, p V2/2.

CALORIC EQUATION OF STATE A caloric equation of state is an equation of the form u=u(v, T) (7) It can be shown that du=c, dT [therm peril (8b) If the gas is calorically perfect--that is, the specific heats are constant--equation (8b) can be integrated to obtain u=c,T+u, [peril (9)

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