Accession Number : AD0616129

Title :   CALCULATION OF PROCESSES IN THE COMBUSTION CHAMBER AND NOZZLE OF A LIQUID-PROPELLANT ROCKET ENGINE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Bolgarskii,A. V.

Report Date : OCT 1959

Pagination or Media Count : 122

Abstract : The book is devoted to questions of combustion and discharge at high temperatures in a liquid-propellant rocket engine. It gives the detailed technique for the thermodynamic calculation of the working process, illustrated by the solution of a series of practical problems. The book offers the bases for the possibility of applying a graphical method for calculating the parameters of the liquid-propellant rocket engine, which greatly facilitates this calculation. It gives a detailed exposition of the technique of constructing such nomograms. Two nomograms for two types of propellant, constructed by the author, are appended at the end of the book. (Author)

Descriptors :   (*LIQUID PROPELLANT ROCKET ENGINES, PERFORMANCE(ENGINEERING)), (*COMBUSTION CHAMBERS, THERMODYNAMICS), (*ROCKET NOZZLES, THERMODYNAMICS), LIQUID ROCKET PROPELLANTS, COMBUSTION, DENSITY, LIQUID ROCKET OXIDIZERS, COMBUSTION CHAMBER GASES, COMBUSTION PRODUCTS, EXHAUST GASES, THERMAL PROPERTIES, NONEQUILIBRIUM FLOW, NUMERICAL ANALYSIS, NOMOGRAPHS, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE