Browse > Article

Buckling Behavior of Stiffened Laminated Composite Cylindrical Panel  

이종선 (대진대학교 기계설계공학과)
원종진 (국민대학교 기계ㆍ자동차공학부)
홍석주 (조선대학교 기계공학과)
윤희중 (인천기능대학 자동화시스템과)
Publication Information
Transactions of the Korean Society of Machine Tool Engineers / v.12, no.5, 2003 , pp. 88-93 More about this Journal
Abstract
Buckling behavior of stiffened laminated composite cylindrical panel was studied using linear and nonlinear deformation theory. Various buckling load factors are obtained for stiffened laminated composite cylindrical panels with rectangular type longitudinal stiffeners and various longitudinal length to radius ratio, which made from Carbon/Epoxy USN150 prepreg and are simply-supported on four edges under uniaxial compression. Buckling behavior design analyses are carried out by the nonlinear search optimizer, ADS.
Keywords
Buckling Behavior; Cylindrical Panel; Axial Compression; Length to Radius Ratio; Membrance Prebuckling;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 A Direct Search Algorithm for Automated Optimum Structural Design /
[ Pappas,M.;Amba-Rao,C.L. ] / AIAA Journal   DOI
2 Weight Comparisons of Optimized Stiffened, Unstiffened, and Sandwich Cylindrical Shells /
[ Agarwal,B.L.;Sobel,L.H. ] / J. Aircraft   DOI   ScienceOn
3 Weight Optimization of Stiffened Cylinders under Axial Compression /
[ Qiu,R. ] / Computers and Structures   DOI   ScienceOn
4 Minimum Weight Design of Stiffened Cylinders under Axial Compression with and without Lateral Pressure /
[ Simites,G.J.;Ungbhakorn,V. ] / Computer & Structure
5 A General Purpose Optimization Program for Engineering Design /
[ Vanderplaats,G.N.;Sugimoto,H. ] / Computers and Structures   DOI   ScienceOn
6 Minimum Weight Design of Stiffened Cylinders under Axial Compression /
[ Simites,G.J.;Ungbhakorn,V. ] / AIAA Journal   DOI   ScienceOn
7 /
[ Zoutendijk,G. ] / Method of Feasible Direction
8 A Preliminary Design Procedure for Composite Panels with Open-Section Stiffeners Loading in the Post-buckling Range /
[ Dickson,J.N.;Biggers,S.B.;Wang,T.S. ] / Advanture in Composite Material
9 Theoretical Basis of the PANDA Computer Program for Preliminary Design of Stiffened Panel under Combined In-Plane Loads /
[ D.Bushnell ] / Computers and Structures   DOI   ScienceOn
10 Pressure Hull Optimization Using General Instability Equation Admitting More Than One Longitudinal Buckling Half-Wave /
[ Pappas,M.;Allentuch,A. ] / Journal of Research
11 Optimal Design of Stiffened Laminate Composite Cylindrical Shells /
[ Won,C.J.;Lee,J.S.;Hong,S.J. ] / Trans. of KSMTE   과학기술학회마을
12 CONMIN - A FORTRAN Program for Constrainted Function Minimization /
[ Vanderplaats,G.N. ] / NASA TM X-62-282, version updated in March 1975
13 General Panel Sizing Computer Code and Its Application to Composite Structural Panels /
[ Anderson,M.S.;Stroud,W.J. ] / AIAA Journal   DOI   ScienceOn