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An Experimental Investigation of Base Pressure on a Body of Revolution at High Thrust Levels and Free Stream Mach Numbers of 1.5 to 2.87
Joseph C. Craft
Charles E. Brazzel
出版
U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate
, 1970
URL
http://books.google.com.hk/books?id=bCNOhvcmLN0C&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
An investigation of axial jet effects on the base and afterbody pressures on a body of revolution has been made at free stream Mach numbers of 1.5, 1.75, 2.00, 2.50 and 2.87. Variations were made in nozzle and afterbody geometry while chamber pressures were varied from zero to 1000 psia. For the larger nozzles, sufficient jet mass flow was emitted to cause boundary layer separation on the body surface.