THE EFFECT OF VARYING SECONDARY STAGNATION TEMPERATURE AND MOLECULAR WEIGHT ON THE SIDE FORCE GENERATED BY GASEOUS INJECTION INTO A SUPERSONIC STREAM.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1969
- Accession Number
- AD0710364
Entities
People
- Russel Allen Chambers
Organizations
- Naval Postgraduate School