Vibration characteristics of a cantilever plate with swept-back leading edge

Heiba, A. E.

dc.contributor.author	Heiba, A. E.
dc.date.accessioned	2013-03-19T16:48:35Z
dc.date.available	2013-03-19T16:48:35Z
dc.date.issued	1982-10
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7872
dc.description.abstract	The paper presents an experimental study of natural frequencies and modes of vibration of uniform cantilever plates. Sixteen planforms are tested by combining aspect ratios of 0.8, 1.2, 1.6 and 2 with leading edge sweep-back angles of 00, 150, 300 and 45°. Experimental values of the natural frequencies for the first six modes are presented for each plate, together with the nodal patterns concerned. The results have been plotted in frequency curves of the same 'family shape'.	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	82	en_UK
dc.title	Vibration characteristics of a cantilever plate with swept-back leading edge	en_UK
dc.type	Report	en_UK