The stress distribution in triangular cantilever plates under a uniform normal load and under a tip load is investigated theoretically. Numerical solutions are presented for plates with angles of sweep from 0 deg. to 60 deg. and with tip angles of 30 deg., 45 deg., 60 deg., 75 deg. and 90 deg.
Stress Analysis of Triangular Cantilever Plates
A Theoretical Investigation using the Inextensional Theory for Thin Plates
Aircraft Engineering and Aerospace Technology ; 27 , 9 ; 287-291
01.09.1955
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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