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Volumn 49, Issue 3, 2011, Pages 448-454

Curvilinear fiber optimization tools for design thin walled beams

Author keywords

Curvilinear fiber; Failure; Non classical effect; Thin walled composite beams; Variable stiffness

Indexed keywords

CURVILINEAR FIBER; FAILURE; NON-CLASSICAL EFFECT; THIN-WALLED COMPOSITE BEAM; VARIABLE STIFFNESS;

EID: 79551593023     PISSN: 02638231     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.tws.2010.08.002     Document Type: Article
Times cited : (30)

References (16)
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    • Z. Gurdal, and R. Olmedo In-plane response of laminates with spatially varying fiber orientations: variable stiffness concept AIAA Journal 31 1993 4
    • (1993) AIAA Journal , vol.31 , pp. 4
    • Gurdal, Z.1    Olmedo, R.2
  • 8
    • 40849141373 scopus 로고    scopus 로고
    • Design of variable-stiffness conical shells for maximum fundamental eigenfrequency
    • A.W. Blom, S. Setoodeh, J. Hol, and Z. Gurdal Design of variable-stiffness conical shells for maximum fundamental eigenfrequency Computers and Structures 86 2008 870 878
    • (2008) Computers and Structures , vol.86 , pp. 870-878
    • Blom, A.W.1    Setoodeh, S.2    Hol, J.3    Gurdal, Z.4
  • 9
    • 0025802403 scopus 로고
    • The shear strain influence on the dynamics of thin-walled beams
    • F. Laudiero, and M. Savoia The shear strain influence on the dynamics of thin-walled beams Thin-Walled Structures 11 1991 375 407
    • (1991) Thin-Walled Structures , vol.11 , pp. 375-407
    • Laudiero, F.1    Savoia, M.2
  • 10
    • 0003894619 scopus 로고    scopus 로고
    • Vibration and aeroelasticity of advanced aircraft wings modeled as thin-walled beamsdynamics
    • PhD thesis, Virginia Polytechnic Institute and State University
    • Qin Z. Vibration and aeroelasticity of advanced aircraft wings modeled as thin-walled beamsdynamics, stability and control. PhD thesis, Virginia Polytechnic Institute and State University, 2001.
    • (2001) Stability and Control
    • Qin, Z.1
  • 12
    • 34548022849 scopus 로고    scopus 로고
    • Flexuraltorsional behavior of thin-walled composite beams with closed cross-section
    • F. Shadmehri, H. Haddadpour, and M.A. Kouchakzadeh Flexuraltorsional behavior of thin-walled composite beams with closed cross-section Thin-Walled Structures 45 2007 699 705
    • (2007) Thin-Walled Structures , vol.45 , pp. 699-705
    • Shadmehri, F.1    Haddadpour, H.2    Kouchakzadeh, M.A.3
  • 13
    • 35548977690 scopus 로고    scopus 로고
    • Mechanics of thin-walled curved beams made of composite materials, allowing for shear deformability
    • T. Piovan Marcelo, and H. Cortinez Victor Mechanics of thin-walled curved beams made of composite materials, allowing for shear deformability Thin-Walled Structures 45 2007 759 789
    • (2007) Thin-Walled Structures , vol.45 , pp. 759-789
    • Piovan, M.T.1    Cortinez, V.H.2
  • 14
    • 45649084430 scopus 로고    scopus 로고
    • Nonlinear aeroelastic response of slender wings based on Wagner function
    • Sh. Shams, M.H. Sadr Lahidjani, and H. Haddadpour Nonlinear aeroelastic response of slender wings based on Wagner function Thin-Walled Structures 46 2008 1192 1203
    • (2008) Thin-Walled Structures , vol.46 , pp. 1192-1203
    • Shams, S.1    Sadr Lahidjani, M.H.2    Haddadpour, H.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.