Some curves for use in calculations of the performance of conical centrebody intakes at supersonic speeds and at full mass flow

dc.contributor.author	L.E. Fraenkel	en_US
dc.date.accessioned	2014-10-20T11:00:10Z
dc.date.available	2014-10-20T11:00:10Z
dc.date.issued	1951	en_US
dc.identifier.other	ARC/CP-108	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/121
dc.description.abstract	This note presents curves of a number of parameters which frequently Occur in calculations of the performance of conical centrebody intakes at supersonic speeds and full mass flow. These parameters follow directly from the theoretical supersonic flow past cones. Semi-cone angles of 15°, 20°, 22.5°, 25°, and 30° are considered, and the range of free stream Mach number is approximately 1.3 to 3.0.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Some curves for use in calculations of the performance of conical centrebody intakes at supersonic speeds and at full mass flow	en_US