The calculation of the velocity distribution due to thickness for swept wings with subsonic edges at supersonic speeds

dc.contributor.author	A. B. Haines	en_US
dc.contributor.author	K. Rollins	en_US
dc.contributor.author	J. Osborn	en_US
dc.date.accessioned	2014-10-20T11:03:20Z
dc.date.available	2014-10-20T11:03:20Z
dc.date.issued	1962	en_US
dc.identifier.other	ARC/CP-654	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/667
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The calculation of the velocity distribution due to thickness for swept wings with subsonic edges at supersonic speeds	en_US