Buckling Behavior of Stiffened Laminated Composite Cylindrical Panel

보강된 복합적층 원통형패널의 좌굴거동

  • 이종선 (대진대학교 기계설계공학과) ;
  • 원종진 (국민대학교 기계ㆍ자동차공학부) ;
  • 홍석주 (조선대학교 기계공학과) ;
  • 윤희중 (인천기능대학 자동화시스템과)
  • Published : 2003.10.01

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

References

  1. AIAA Journal v.13 no.6 Minimum Weight Design of Stiffened Cylinders under Axial Compression Simites,G.J.;Ungbhakorn,V. https://doi.org/10.2514/3.60432
  2. Computer & Structure v.8 Minimum Weight Design of Stiffened Cylinders under Axial Compression with and without Lateral Pressure Simites,G.J.;Ungbhakorn,V.
  3. AIAA Journal v.9 A Direct Search Algorithm for Automated Optimum Structural Design Pappas,M.;Amba-Rao,C.L. https://doi.org/10.2514/3.6192
  4. Journal of Research v.19 Pressure Hull Optimization Using General Instability Equation Admitting More Than One Longitudinal Buckling Half-Wave Pappas,M.;Allentuch,A.
  5. AIAA Journal v.17 General Panel Sizing Computer Code and Its Application to Composite Structural Panels Anderson,M.S.;Stroud,W.J. https://doi.org/10.2514/3.61242
  6. Method of Feasible Direction Zoutendijk,G.
  7. NASA TM X-62-282, version updated in March 1975 CONMIN - A FORTRAN Program for Constrainted Function Minimization Vanderplaats,G.N.
  8. J. Aircraft v.14 no.10 Weight Comparisons of Optimized Stiffened, Unstiffened, and Sandwich Cylindrical Shells Agarwal,B.L.;Sobel,L.H. https://doi.org/10.2514/3.58885
  9. Advanture in Composite Material v.1 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.
  10. Computers and Structures v.27 no.4 Theoretical Basis of the PANDA Computer Program for Preliminary Design of Stiffened Panel under Combined In-Plane Loads D.Bushnell https://doi.org/10.1016/0045-7949(87)90280-X
  11. Computers and Structures v.21 no.5 Weight Optimization of Stiffened Cylinders under Axial Compression Qiu,R. https://doi.org/10.1016/0045-7949(85)90206-8
  12. Computers and Structures v.24 A General Purpose Optimization Program for Engineering Design Vanderplaats,G.N.;Sugimoto,H. https://doi.org/10.1016/0045-7949(86)90331-7
  13. Trans. of KSMTE v.7 no.6 Optimal Design of Stiffened Laminate Composite Cylindrical Shells Won,C.J.;Lee,J.S.;Hong,S.J.