The aerodynamic derivatives with respect to sideslip for a delta wing with small dihedral at supersonic speeds

Robinson, A.; Hunter-Tod, J. H.

dc.contributor.author	Robinson, A.
dc.contributor.author	Hunter-Tod, J. H.
dc.date.accessioned	2012-05-08T19:30:26Z
dc.date.available	2012-05-08T19:30:26Z
dc.date.issued	1947-12
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7128
dc.description.abstract	Expressions are derived for the sideslip derivatives on the assumptions of the linearised theory of flow for a delta wing with small dihedral flying at supersonic speeds. A discussion is included in the appendix on the relation between two methods that have been evolved for the treatment of aerodynamic force problems of the delta wing lying within its apex Mach cone. Continues…	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	12	en_UK
dc.title	The aerodynamic derivatives with respect to sideslip for a delta wing with small dihedral at supersonic speeds	en_UK
dc.type	Report	en_UK