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An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack
Robert H. Feldhuhn
Lionel Pasiuk
出版
United States Naval Ordnance Laboratory
, 1968
URL
http://books.google.com.hk/books?id=IMc5w-2W724C&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.
