Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing

dc.contributor.author	L. Pennelegion	en_US
dc.contributor.author	R. F. Cash	en_US
dc.date.accessioned	2014-10-20T11:03:42Z
dc.date.available	2014-10-20T11:03:42Z
dc.date.issued	1963	en_US
dc.identifier.other	ARC/CP-684	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/697
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing	en_US