Slot jet interaction studies of an ogive cylinder at M[infinity] = 4 and 5 /
by David L. Merritt, Philip M. Aronson.
Description
- Language(s)
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English
- Published
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White Oak, Maryland : United States Naval Ordnance Laboratory, 1968.
- Summary
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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).
- Note
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"10 September 1968".
- Physical Description
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iv, 22 [30] pages :
illustrations;
28 cm.
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