Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3

dc.contributor.author	P. R. Guyett	en_US
dc.contributor.author	J. K. Curran	en_US
dc.date.accessioned	2014-10-21T15:54:58Z
dc.date.available	2014-10-21T15:54:58Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/R&M-3171	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3740
dc.description.abstract	A complete set of oscillatory aerodynamic stiffness and damping derivatives has been determined for a rectangular wing for rigid-wing modes of normal translation, pitch, and roll, in the range of frequency parameter 0.4 to 1.3, at low subsonic wind speeds. Each available comparison shows that the results are in satisfactory agreement with theoretical derivatives calculated by W. P. Jones and by Lawrence and Gerber.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3	en_US