The influence of design pressure ratio and divergence angle on the thrust of convergent-divergent propelling nozzles

dc.contributor.author	P. F. Ashwood	en_US
dc.contributor.author	D. G. Higgins	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-325	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/338
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The influence of design pressure ratio and divergence angle on the thrust of convergent-divergent propelling nozzles	en_US