Wind Tunnel Tests on Six Wing-Body Models at M=4.

Wind Tunnel Tests on Six Wing-Body Models at M=4.
by J. Pike.
Aeronautical Research Council, Current Paper Number 1074, Ministry of Technology, HMSO, London, Aug 1967.

Summary.
Force measurements and flow patterns for six models, with the same ogive-cylinder body and various wings, are presented for a free stream Mach number of 4. Five of the wings were unswept, and the sixth was a 65 degree delta. Values of CL, Cm and CD are compared for models of different wing section, aspect ratio and taper ratio. They are also compared with values from the same models tested at lower Mach numbers.

Availability.
Download ARC CP1074
or email J A C K @ J A C K P I K E . C O . U K

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Last amended: Dec 2013.