Wind tunnel tests on six wing-body models at M = 4

dc.contributor.author	J. Pike	en_US
dc.date.accessioned	2014-10-20T11:05:33Z
dc.date.available	2014-10-20T11:05:33Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/CP-1074	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1087
dc.description.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.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Wind tunnel tests on six wing-body models at M = 4	en_US