메뉴 건너뛰기




Volumn 83, Issue 19-20, 2005, Pages 1546-1554

Optimal design of composite wing subjected to gust loads

Author keywords

Branch and bound method; Gust loads; Monte Carlo simulation; Stacking sequence

Indexed keywords

CANTILEVER BEAMS; COMPOSITE MATERIALS; COMPUTER SIMULATION; MONTE CARLO METHODS; NUMERICAL METHODS; PROBABILITY; STRAIN; STRUCTURAL DESIGN; WIND EFFECTS;

EID: 19944388589     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2005.02.002     Document Type: Article
Times cited : (69)

References (17)
  • 1
    • 0018505973 scopus 로고
    • Preliminary design of composite wings for buckling, strength, and displacement constraints
    • J.H. Starnes, and R.T. Haftka Preliminary design of composite wings for buckling, strength, and displacement constraints J Aircraft 16 1979 564 570
    • (1979) J Aircraft , vol.16 , pp. 564-570
    • Starnes, J.H.1    Haftka, R.T.2
  • 2
    • 0018431325 scopus 로고
    • An efficient structural resizing procedure for meeting static aeroelastic design objectives
    • E. Lerner, and J. Markowitz An efficient structural resizing procedure for meeting static aeroelastic design objectives J Aircraft 16 1979 65 71
    • (1979) J Aircraft , vol.16 , pp. 65-71
    • Lerner, E.1    Markowitz, J.2
  • 3
    • 0026056481 scopus 로고
    • Optimum design of composite wing structures by a refined optimality criterion
    • I.W. Liu, and C.C. Lin Optimum design of composite wing structures by a refined optimality criterion Compos Struct 17 1991 51 65
    • (1991) Compos Struct , vol.17 , pp. 51-65
    • Liu, I.W.1    Lin, C.C.2
  • 4
    • 0034294331 scopus 로고    scopus 로고
    • Two-level composite wing structural optimization using response surface
    • B. Liu, R.T. Haftka, and M.A. Akgün Two-level composite wing structural optimization using response surface Struct Multidisc Optimiz 20 2000 87 96
    • (2000) Struct Multidisc Optimiz , vol.20 , pp. 87-96
    • Liu, B.1    Haftka, R.T.2    Akgün, M.A.3
  • 6
    • 19944388132 scopus 로고
    • A revised formula for the calculation of gust loads
    • Pratt KG. A revised formula for the calculation of gust loads. NACA TN 2964, 1953
    • (1953) NACA TN , vol.2964
    • Pratt, K.G.1
  • 7
    • 19944424016 scopus 로고
    • Code of Federal Regulations No. 14
    • Code of Federal Regulations No. 14, Aeronautics and Space, part 25, 1993
    • (1993) Aeronautics and Space, Part 25
  • 12
    • 0021128188 scopus 로고
    • Design of laminated plates for maximum stiffness
    • T.R. Tauchert, and S. Adibhalta Design of laminated plates for maximum stiffness J Compos Mater 18 1984 58 69
    • (1984) J Compos Mater , vol.18 , pp. 58-69
    • Tauchert, T.R.1    Adibhalta, S.2
  • 13
    • 0029712166 scopus 로고    scopus 로고
    • Object-oriented approach to optimize composite laminated plate stiffness with discrete ply angles
    • A. Todoroki, N. Sasada, and M. Miki Object-oriented approach to optimize composite laminated plate stiffness with discrete ply angles J Compos Mater 30 1996 1020 1041
    • (1996) J Compos Mater , vol.30 , pp. 1020-1041
    • Todoroki, A.1    Sasada, N.2    Miki, M.3
  • 14
    • 0034778903 scopus 로고    scopus 로고
    • Optimal design of composite laminated plates with the discreteness in ply angles and uncertainty in material properties considered
    • T.U. Kim, and H.C. Sin Optimal design of composite laminated plates with the discreteness in ply angles and uncertainty in material properties considered Comput Struct 79 2001 2501 2509
    • (2001) Comput Struct , vol.79 , pp. 2501-2509
    • Kim, T.U.1    Sin, H.C.2
  • 17
    • 0027595481 scopus 로고
    • Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
    • R.L. Riche, and R.T. Haftka Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm AIAA J 31 1994 951 956
    • (1994) AIAA J , vol.31 , pp. 951-956
    • Riche, R.L.1    Haftka, R.T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.