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Volumn 70, Issue 1, 1998, Pages 4-8

The optimisation of wing structures - Theory or practice?

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; COMPUTER SOFTWARE; DESIGN; DYNAMIC RESPONSE; OPTIMIZATION; PARAMETER ESTIMATION; COMPUTER AIDED DESIGN; FLUTTER (AERODYNAMICS); STRUCTURAL OPTIMIZATION; VIBRATIONS (MECHANICAL); WINGS;

EID: 0031700314     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022669810196000     Document Type: Article
Times cited : (4)

References (31)
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    • Banerjee, J.R.1    Williams, F.W.2
  • 6
    • 0023167129 scopus 로고
    • PANDA2 -program for minimum weight design of stiffened, composite, locally buckled panels"
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    • Bushnell, D.1
  • 7
    • 0029305851 scopus 로고
    • Optimum design of composite stiffened wing panels - A parametric study"
    • Butler, R. (1995), "Optimum design of composite stiffened wing panels - a parametric study". The Aeronautical Journal, Vol. 99 No. 985, pp. 169-77.
    • (1995) The Aeronautical Journal , vol.99 , Issue.985 , pp. 169-177
    • Butler, R.1
  • 9
    • 0026861361 scopus 로고
    • Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates"
    • Butler, R. and Williams, F.W. (1992), "Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates". Computers & Structures, Vol. 43 No. 4, pp. 699-708.
    • (1992) Computers & Structures , vol.43 , Issue.4 , pp. 699-708
    • Butler, R.1    Williams, F.W.2
  • 12
    • 0026835516 scopus 로고
    • Stacking-sequence optimization for buckling of laminated plates by integer programming"
    • Haftka, R.T. and Walsh, J.L. (1992), "Stacking-sequence optimization for buckling of laminated plates by integer programming", AIM Journal. Vol. 30 No. 3, pp. 814-19.
    • (1992) AIM Journal. , vol.30 , Issue.3 , pp. 814-819
    • Haftka, R.T.1    Walsh, J.L.2
  • 14
    • 0031061903 scopus 로고    scopus 로고
    • Aeroelastic optimisation of composite wings using the dynamic stiffness method"
    • Lillico, M., Butler, R., Guo, S.J. and Banerjee, J.R. (1997), "Aeroelastic optimisation of composite wings using the dynamic stiffness method". The Aeronautical Journal, Vol. 101 No. 1002, pp. 77-86.
    • (1997) The Aeronautical Journal , vol.101 , Issue.1002 , pp. 77-86
    • Lillico, M.1    Butler, R.2    Guo, S.J.3    Banerjee, J.R.4
  • 18
    • 0001694169 scopus 로고
    • The limits of economy of material in frame structures"
    • Michell, A.G.M. (1904), "The limits of economy of material in frame structures". Philosophical Magazine, Series 6, Vol. 8 No. 47, pp. 589-95.
    • (1904) Philosophical Magazine, Series 6 , vol.8 , Issue.47 , pp. 589-595
    • Michell, A.G.M.1
  • 28
    • 34250076701 scopus 로고
    • Multiparameter structural optimization using FEM and multi-point explicit approximations"
    • Toropov, V., Filatov, A.A. and Polynkin, A.A. (1993), "Multiparameter structural optimization using FEM and multi-point explicit approximations". Structural Optimization, Vol. 6, pp. 7-14.
    • (1993) Structural Optimization , vol.6 , pp. 7-14
    • Toropov, V.1    Filatov, A.A.2    Polynkin, A.A.3
  • 29
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    • Colorado Springs, CO.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.