Measurements of oscillatory derivatives at mach numbers up to 2.6 on a model of a supersonic transport design study (Bristol type 198)

dc.contributor.author	J. S. Thompson	en_US
dc.contributor.author	R. A. Fail	en_US
dc.date.accessioned	2014-10-20T11:04:19Z
dc.date.available	2014-10-20T11:04:19Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/CP-815	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/828
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Measurements of oscillatory derivatives at mach numbers up to 2.6 on a model of a supersonic transport design study (Bristol type 198)	en_US