Measurements of pitching-moment derivatives for blunt-nosed aerofoils oscillating in two-dimensional supersonic flow

dc.contributor.author	P. G. Pugh	en_US
dc.contributor.author	L. Woodgate	en_US
dc.date.accessioned	2014-10-21T15:55:51Z
dc.date.available	2014-10-21T15:55:51Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3315	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3895
dc.description.abstract	Direct pitching-moment derivatives have been measured using the method of Scruton, Woodgate et al for two single-wedge blunt-nosed aerofoils. These measurements were made at Mach numbers of 1.75 and 2.47 and frequency parameters less than 0.02. In general, nose blunting was found to have little effect on the derivatives although changes were observed for the thinner wedge at a Mach number of 1.75.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Measurements of pitching-moment derivatives for blunt-nosed aerofoils oscillating in two-dimensional supersonic flow	en_US