Accession Number : AD0710364

Title :   THE EFFECT OF VARYING SECONDARY STAGNATION TEMPERATURE AND MOLECULAR WEIGHT ON THE SIDE FORCE GENERATED BY GASEOUS INJECTION INTO A SUPERSONIC STREAM.

Descriptive Note : Master's thesis,

Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s) : Chambers,Russel Allen

Report Date : OCT 1969

Pagination or Media Count : 47

Abstract : The study was undertaken to investigate the effects of varying the injectant temperature and molecular weight on the flow field generated by the interaction of a secondary jet with a supersonic mainstream. The experimental portions of this investigation were conducted at a primary Mach number of 1.92. Data are presented and compared with theory. The presentation includes correlation of the penetration height of the secondary flow, interaction side force amplification factor, and separation distance non-dimensionalized with respect to the penetration height. (Author)

Descriptors :   (*CONTROL JETS, INJECTION), (*FORCE(MECHANICS), JET MIXING FLOW), SUPERSONIC FLOW, MOLECULAR WEIGHT, STAGNATION POINT, TEMPERATURE, GUIDED MISSILES, SECONDARY FLOW, THESES

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE