The influence of pressure ratio and divergence angle on the shock position in two dimensional, over-expanded, convergent-divergent nozzles

dc.contributor.author	P. F. Ashwood	en_US
dc.contributor.author	G. W. Crosse	en_US
dc.date.accessioned	2014-10-20T11:01:17Z
dc.date.available	2014-10-20T11:01:17Z
dc.date.issued	1957	en_US
dc.identifier.other	ARC/CP-327	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/340
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The influence of pressure ratio and divergence angle on the shock position in two dimensional, over-expanded, convergent-divergent nozzles	en_US