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Slot Jet Interaction Studies of an Ogive Cylinder at M[infinity]
Ralph Edward PhinneyMichael J WerleJ. KnottW. C. Volz
出版United States Naval Ordnance Laboratory, 1968
URLhttp://books.google.com.hk/books?id=u_2ZjqmUfeUC&hl=&source=gbs_api
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註釋An experimental study of the control forces and moments generated by a slot-type secondary jet located near the base of an ogive cylinder in a Mach 4 and 5 free stream was conducted in the NOL Supersonic Tunnel No. 2. The free-stream Reynolds number, based on body length, was held constant at 22,000,000 and the missile angle of attack was varied from -10 to +10 degrees. The jet slot spanned one quadrant of the cylindrical surface and was contained between two low aspect ratio fins. (Author).