The hemispherical, differential pressure yawmeter at supersonic speed

dc.contributor.author	L. J. Beecham	en_US
dc.date.accessioned	2014-10-21T15:55:30Z
dc.date.available	2014-10-21T15:55:30Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/R&M-3237	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3811
dc.description.abstract	Available data on the pressure distribution around a hemisphere at supersonic speeds are reviewed with special reference to the differential pressure. A modified form of pressure coefficient is used which collapses the data down to low supersonic speeds, and suggests that the normalised yawmeter sensitivity can be made virtually independent of Mach number by suitable orifice location.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The hemispherical, differential pressure yawmeter at supersonic speed	en_US