Slot Jet Interaction Studies of an Ogive Cylinder at M = 4 and 5.
Abstract
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 10, 1968
- Accession Number
- AD0845933
Entities
People
- J. Knott
- M. J. Werle
- R. E. Phinney
- W. C. Volz
Organizations
- Naval Ordnance Laboratory