A momentum analysis of lifting surfaces in inviscid supersonic flow

dc.contributor.author	P. L. Roe	en_US
dc.date.accessioned	2014-10-21T15:49:56Z
dc.date.available	2014-10-21T15:49:56Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/R&M-3576	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2843
dc.description.abstract	Momentum considerations are used to derive relationships between the lifting efficieny of a wing having an attached shock system and properties of the flow field around it. Optimum two-dimensional flow fields are derived using shock expansion theory. These may be used to design three-dimensional shapes having slightly greater lifting efficiencies than plane wedges. An analysis of the flow in any plane of symmetry is used to suggest desirable features of more general flow fields.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A momentum analysis of lifting surfaces in inviscid supersonic flow	en_US