Abstract
Tables of functions are given for solving problems in one-dimensional, compressible gas flow when energy effects, as represented by changes in stagnation temperature, are involved. The tables may be used for such typical processes as heat transfer at high gas speeds, combustion, moisture condensation shocks, flame fronts, and detonation waves. The Mach number is the independent argument of the tables, and there is one table for each of six specific-heat ratios, namely, 1.0, 1.1, 1.2, 1.3, 1.4, and 1.67.