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Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model

其他書名	Flows over full span ramps mounted on a flat plate. Part III
出版	AF Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1964
URL	http://books.google.com.hk/books?id=IlLo4rY9hXEC&hl=&source=gbs_api

註釋The report presents data obtained on the upper, flat plate, surface of the model and on the face of a 25% chord, full span, ramp mounted on the trailing edge of the flat plate. Data were obtained for three ramp angles, both with and without internal cooling of the flat plate surface, for model angles of attack from -43 to +10 degrees for free stream Reynolds numbers per foot of 1.1, 2.2 and 3.3 million.