Design and operating features of the N.P.L. 6 in. shock tunnel

dc.contributor.author	L. Pennelegion	en_US
dc.contributor.author	R. F. Cash	en_US
dc.contributor.author	D. F. Bedder	en_US
dc.date.accessioned	2014-10-21T15:56:30Z
dc.date.available	2014-10-21T15:56:30Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/R&M-3449	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/4030
dc.description.abstract	Engineering aspects of the shock tunnel facility are described. Details of gas services and routine instrumentation are given. The performance envelope of the tunnel is discussed and routine measurements presented.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Design and operating features of the N.P.L. 6 in. shock tunnel	en_US