An investigation of the flow over a half-wing model with 60.5 degrees leading edge sweepback, at a high subsonic and supersonic speeds

dc.contributor.author	F. O'Hara	en_US
dc.contributor.author	J. B. Scott-Wilson	en_US
dc.date.accessioned	2014-10-20T11:02:00Z
dc.date.available	2014-10-20T11:02:00Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/CP-471	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/484
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	An investigation of the flow over a half-wing model with 60.5 degrees leading edge sweepback, at a high subsonic and supersonic speeds	en_US