Accession Number : AD0645634

Title :   COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET ENGINES.

Descriptive Note : Final rept.,

Corporate Author : POLYTECHNIC INST OF BROOKLYN N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS

Personal Author(s) : Agosta,Vito D. ; Hammer,Sanford S.

Report Date : OCT 1966

Pagination or Media Count : 22

Abstract : The investigation is concerned with the development of a theoretical model for combustion instability, in the longitudinal mode, occurring in liquid propellant rocket engines that are employed in current practice. Experimental results are used both to help generate realistic physical models for combustion-wave phenomena in heterogeneously reacting systems, and for subsequent verification of theoretical results. (Author)

Descriptors :   (*LIQUID PROPELLANT ROCKET ENGINES, COMBUSTION), (*COMBUSTION, STABILITY), MATHEMATICAL MODELS, DROPS, EVAPORATION, BIPROPELLANTS, OSCILLATION

Subject Categories : Combustion and Ignition
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE