日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
截頭円錐殼の軸圧縮挫屈に関する一実験
児島 一雄市田 和夫砂川 恵
著者情報
ジャーナル フリー

1973 年 21 巻 228 号 p. 32-38

詳細
抄録

Using the seamless specimen made of PMMA sheet by a vacuum-forming process at elevated temperature, an experimental investigation on tne buckling of imperfect truncated conical shells under axial compression is carried out. The imperfection implies here that the thickness of specimen is uniform in the circumferential direction and varies nearly linearly along its generating line. It is shown that the empirical formula given by WEINGARTEN et al. can be used conservatively in the design of imperfect truncated conical shells mentioned above representing their thickness by the mean value, and the initiation and propagation of buckling deformation are discussed. too.

著者関連情報
© The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top