TABLES OF THERMODYNAMIC FUNCTIONS FOR ANALYSIS OF AIRCRAFT-PROPULSION SYSTEMS

摘要

Tables of thermodynamic functions are presented for 42 sub¬stances containing the following elements: argon, aluminum, boron, carbon, chlorine, fluorine, hydrogen, lithium, nitrogen, and oxygen. The functions tabulated are specific heat at constant pressure Cp°, sensible enthalpy HT-H00, sum of sensible enthalpy and chemical energy HT, molar entropy ST, enthalpy change due to formation of substance from elements in atomic gas state divided by gas con¬stant times temperature -AH°/ET, and the logarithm of the equilib¬rium constant log10 K at temperatures of 298.16° K and every 100° from 300° to 6000° K.