任意後退角を有する変厚後退片持平板の曲げ応力解析

概要

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A numerical method is presented for the problem of the bending stress of thin elastic cantilevered plate of variable thickness, having arbitrary swept-back angle and taper and being subjected to the pressure load on its surface and the temperature distribution in itself. Three examples are solved by relaxation method; Examples 1 and 2 treat the solid wing plates of variable thickness and swept angle of tan^<-1>(3/4). The former is supported simply at four points and the latter is fixed at the root. Example 3 treats the tapered solid wing plate which is fixed at the root. For all of these examples the loads are assumed to be uniformly distributed. Furthermore, experiments for the above three examples are carried out. Fair agreement is observed between the numerical and the experimental results.
一般社団法人日本機械学会の論文
1963-10-25