Institute of Space and Aeronautical Science, University of Tokyo
Institute of Space and Aeronautical Science, University of Tokyo
Institute of Space and Aeronautical Science, University of Tokyo
The purpose of this paper is to report the recent developments of the study of the zeta-stiffened panel. First, the mechanism of stiffening by a doublly corrugated plate is explained in some details and then, the guiding principle of optimizing the zeta-stiffened panel. The automation of fabricating the structural model of compicated configuration, such as this panel, by use of the NC machine is also discussed in the paper.
<論文>ZETA補強板の設計
SA0125858.pdf
(1.55MB)
