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

dc.contributor.authorHeiba, A. E.
dc.date.accessioned2013-03-19T16:48:35Z
dc.date.available2013-03-19T16:48:35Z
dc.date.issued1982-10
dc.description.abstractThe 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7872
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfield.en_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries82en_UK
dc.titleVibration characteristics of a cantilever plate with swept-back leading edgeen_UK
dc.typeReporten_UK

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
COA_Report_No_82_Oct_1954.pdf
Size:
5.04 MB
Format:
Adobe Portable Document Format
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:

Collections