Accession Number : AD0600298

Title :   AN EXACT METHOD OF CALCULATING HEAT CAPACITIES AT HIGH TEMPERATURES AND APPLICATIONS IN GASDYNAMICAL RELATIONSHIPS.

Descriptive Note : Technical note,

Corporate Author : BROWN ENGINEERING CO INC HUNTSVILLE ALA

Personal Author(s) : Walter,Benno ; Walter,Hans

Report Date : FEB 1964

Pagination or Media Count : 39

Abstract : Fundamental gasdynamical relationships at high temperatures are developed. The relationships differ from the classical formulations mainly in that the heat capacities as well as their ratios are no longer assumed constant but rather depend on the temperature. The presented methods are of specific applicability in propulsion by high energy propellants as well as by nuclear heated hydrogen. (Author)

Descriptors :   (*ROCKET PROPELLANTS, EXHAUST GASES), (*EXHAUST GASES, FLUID DYNAMICS), THERMODYNAMICS, SPECIFIC HEAT, HIGH TEMPERATURE, GAS FLOW, EQUATIONS OF STATE

Distribution Statement : APPROVED FOR PUBLIC RELEASE