Theoretical stability derivatives of a highly swept delta wing and slender body combination

Nonweiler, T.

dc.contributor.author	Nonweiler, T.
dc.date.accessioned	2012-07-04T11:23:38Z
dc.date.available	2012-07-04T11:23:38Z
dc.date.issued	1951-11
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7339
dc.description.abstract	The stability derivatives of a delta wing of small aspect ratio, mounted on a cylindrical body with a slender pointed head, are derived by considering the flow in planes perpendicular to the body axis to be uninfluenced by the change in the streamwise component of the air velocity (the so-called ‘slender body’ theory).	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	50	en_UK
dc.title	Theoretical stability derivatives of a highly swept delta wing and slender body combination	en_UK
dc.type	Report	en_UK