The correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds

dc.contributor.author	M. J. Larcombe	en_US
dc.date.accessioned	2014-10-20T11:05:33Z
dc.date.available	2014-10-20T11:05:33Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1072	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1085
dc.description.abstract	A method for calculating the pressure distributions around conical bodies at high supersonic speeds, based on a local cone-flow theory, has been developed from the successful correlation of pressures at a symmetrical ridge line. The method is shown to provide a means for the accurate estimation of pressures on compression surfaces of conical bodies with sharp leading edges, providing the shock wave is detached from the edge.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds	en_US