The change in shock-tunnel tailoring mach number due to driver gas mixtures of helium and nitrogen

dc.contributor.author	L. Pennelegion	en_US
dc.contributor.author	P.J. Gough	en_US
dc.date.accessioned	2014-10-21T15:56:19Z
dc.date.available	2014-10-21T15:56:19Z
dc.date.issued	1963	en_US
dc.identifier.other	ARC/R&M-3398	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3980
dc.description.abstract	The undoubted advantage of using a reflected-shock tunnel in the tailored condition is the gain in the duration of the steady stagnation and test-section pressures. The resulting increase in testing time of perhaps five times has enabled measurements to be made with force balances and pressure transducers in wind-tunnel models, which have an inherently slow response when considered in terms of 'straight-through' shock-tube testing times.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The change in shock-tunnel tailoring mach number due to driver gas mixtures of helium and nitrogen	en_US