High reynolds number tests on a 70 degrees L.E. sweepback delta wing and body (H.P. 100) in the compressed air tunnel

dc.contributor.author	R. W. F. Gould	en_US
dc.contributor.author	C. F. Cowdrey	en_US
dc.date.accessioned	2014-10-20T11:01:48Z
dc.date.available	2014-10-20T11:01:48Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/CP-387	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/400
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	High reynolds number tests on a 70 degrees L.E. sweepback delta wing and body (H.P. 100) in the compressed air tunnel	en_US