Increased use of heavy wing skins, resulting from various aero-structural considerations at high speed, has necessitated more exact plate instability calculations; determination of critical compression stress and effective width of panels that are stiffened by stringer elements fastened along unloaded edges is discussed.
Effective width of elastically supported flat plates
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 10
1946
7 pages
Bibliography
Article (Journal)
English
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Effective width of elastically supported flat plates
Engineering Index Backfile | 1947
|Fluter analysis of two parallel elastically coupled flat plates
TIBKAT | 1975
|