Performance estimates for a reflected-shock tunnel with a modified driver to produce high test-section Reynolds numbers

dc.contributor.author	J. G. Woodley	en_US
dc.date.accessioned	2014-10-20T11:05:31Z
dc.date.available	2014-10-20T11:05:31Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1057	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1070
dc.description.abstract	Some calculations based on the performance of an ideal shock-tube are presented. These demonstrate the possibility of achieving a high test-section Reynolds number in a reflected-shock tunnel, employing nitrogen or air as the test gas, by the use of a driver gas composed of a mixture of hydrogen and nitrogen.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Performance estimates for a reflected-shock tunnel with a modified driver to produce high test-section Reynolds numbers	en_US