导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (5): 271-276.
• 论文 • Previous Articles Next Articles
Wang Hu, Wang Tsunkuei
Received:
Revised:
Online:
Published:
Abstract: In this paper, a new theory is developed for large deflection of closely stiffened truncated laminated composite conical shells under arbitrary loads by using the variational calculus and smeared-stiffener theory. The most general bending-stretching coupling, the effect of eccentricity of stiffeners and initial deflection are considered. The new equations of the mixed type of the shell are obtained in terms of the transverse deflection and stress function and can be used to solve the problems of stress analysis, deflection, stability and vibration of the shell. The simplified equations are also given for some particular cases.
Key words: composite shell, etrical nonlinearity, large deflection stiffened shell, conical shell, geom-equations
Wang Hu;Wang Tsunkuei. THE LARGE DEFLECTION EQUATIONS OF STIFFENED LAMINATED COMPOSITE CONICAL SHELLS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(5): 271-276.
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y1990/V11/I5/271