Finite element stress analysis of clamped honeycomb sandwich plate under uniformly distributed load = 유한요소법에 의한 분포하중을 받는 고정지지된 Honeycomb sandwich 평판의 응력해석

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A finite element computer program for the stress analysis of honeycomb sandwich structure is developed. This program can treat sandwich plate and shell with anisotropic faces and core of nonconstant thickness. Computational results are presented for stress distributions of a clamped honeycomb sandwich plate subjected to uniformly distributed load. Attention was given to the effect of the change of core property on face stresses. It is found that face stresses are affected by the change of shear modulus and the orientation of principal material axes of core. In orthotropic face sandwich, structurally desirable orientation of core principal material axes is one at which the strong axis of face is aligned with the strong axis of core.
Advisors
Hong, Chang-Sunresearcher홍창선researcher
Description
한국과학기술원 : 항공공학과,
Publisher
한국과학기술원
Issue Date
1983
Identifier
63631/325007 / 000811239
Language
eng
Description

학위논문(석사) - 한국과학기술원 : 항공공학과, 1983.2, [ ii, 56 p. ]

URI
http://hdl.handle.net/10203/26575
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=63631&flag=dissertation
Appears in Collection
AE-Theses_Master(석사논문)
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