Slot jet interaction studies of an ogive cylinder at M[infinity] = 4 and 5 /
by David L. Merritt, Philip M. Aronson.

Description

Main Author

Phinney, R. E. (Ralph Edward)

Related Names

Volz, W. C., author.
Knott, J., author.
Werle, Michael J, author.
Naval Ordnance Laboratory (White Oak, Md.)

Language(s)

English

Published

White Oak, Maryland : United States Naval Ordnance Laboratory, 1968.

Subjects

Aerodynamics, Supersonic.
Guided missiles > Guided missiles / Attitude control systems.

Summary

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

"10 September 1968".

Physical Description

iv, 22 [30] pages : illustrations; 28 cm.

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