Accession Number : AD0632087
Title : PARAMETRIC STUDY OF ROCKET INSTABILITY.
Descriptive Note : Final rept.,
Corporate Author : PURDUE UNIV LAFAYETTE IND SCHOOL OF MECHANICAL ENGINEERING
Personal Author(s) : Osborn,J. R.
Report Date : 10 JAN 1966
Pagination or Media Count : 7
Abstract : The research program was concerned with the determination of those dimensionless parameters that may be employed as criteria for predicting the stability of combustion in a thrust chamber. These dimensionless parameters are related to physical and chemical variables which are available to the design engineer. Both analytical and experimental work were performed to enable the prediction of combustion pressure oscillations and, therefore, avoid them in actual rocket engine design. (Author)
Descriptors : (*ROCKET ENGINES, COMBUSTION), (*COMBUSTION, STABILITY), COMBUSTION CHAMBERS, ROCKET PROPELLANTS, BURNING RATE, FLAME PROPAGATION, PRESSURE, OSCILLATION, THERMODYNAMICS
Subject Categories : Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE