Abstract:
Force measurements and flow patterns for six models, with the same ogive-cylinder body and various wings, are presented for a free streem Mach number of 4. Five of the wings were unswept, and the sixth was a 65° 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.
