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Volumn 35, Issue 3, 1997, Pages 540-545

Optimum design and validation of flat composite beams subject to frequency constraints

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[No Author keywords available]

Indexed keywords


EID: 0343186315     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.128     Document Type: Article
Times cited : (8)

References (16)
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  • 3
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  • 4
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    • Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite/Epoxy Cantilevered Plates
    • Hollowell, S. J., and Dugundji, J., "Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite/Epoxy Cantilevered Plates," Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 69-76.
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  • 6
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  • 7
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    • Grandhi, R.V.1    Bharatram, G.2    Venkayya, V.B.3
  • 8
    • 0030196564 scopus 로고    scopus 로고
    • Optimum Design of Bending-Torsion Coupled Beams with Frequency or Aeroelastic Constraints
    • Butler, R., and Banerjee, J. R., "Optimum Design of Bending-Torsion Coupled Beams with Frequency or Aeroelastic Constraints," Computers and Structures, Vol. 60, No. 5, 1996, pp. 715-724.
    • (1996) Computers and Structures , vol.60 , Issue.5 , pp. 715-724
    • Butler, R.1    Banerjee, J.R.2
  • 9
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    • Free Vibration of Composite Beams - An Exact Method Using Symbolic Computation
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    • Banerjee, J.R.1    Williams, F.W.2
  • 13
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    • A General Algorithm for Computing Natural Frequencies of Elastic Structures
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.