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Wind Tunnel Testing of Interactions of High Altitude Rocket Plumes with the Free Stream

H. K. SmithsonL. L. PriceD. L. Whitfield

出版	Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971
URL	http://books.google.com.hk/books?id=RpFyofWbVscC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

Interactions of model rocket plumes and the free stream at varying simulated altitudes have been investigated in an altitude simulation chamber. Free-stream variables were Mach number, gas, total temperature, and total pressure. Model rocket parameter variables were exhaust gas, area ratio, chamber total pressure and total temperature, and the orientation of the model relative to the free stream. In addition to pitot probe measurements, plume photographs and density measurements were obtained using the electron beam technique. (Author).