日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
複合材積層曲面板上に作用する点衝撃の位置および荷重履歴の同定
小野崎 徹関根 英樹
著者情報
ジャーナル フリー

2002 年 50 巻 586 号 p. 444-450

詳細
抄録

In a previous paper, the authors presented the identification method of locations and force histories of point impacts on laminated composite flat plates by using the measured values of acceleration. This paper deals with an attempt to extend the method so as to apply to identification of point impacts on laminated composite curved panels. Numerical identification results are obtained for the single point impact and double point impacts on cross-ply laminated composite curved panels. The validity of the identification method to laminated composite curved panels is verified by comparing the identification results with exact ones. In addition, when the number of point impacts is unknown, a method to decide the identification results is proposed. Several numerical examples are considered to ascertain the validity of the proposed method.

著者関連情報
© 2002 The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top