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Volumn 11, Issue 5, 2007, Pages 396-404

Aeroelastic optimization of an aerobatic aircraft wing structure

Author keywords

Aeroelastic tailoring; Composite wing box; Laminate layup; Optimization

Indexed keywords

FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); NUMERICAL METHODS; STRESS ANALYSIS; WINGS;

EID: 34249280594     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2007.01.003     Document Type: Article
Times cited : (99)

References (26)
  • 1
    • 0029380374 scopus 로고
    • Free vibration analysis of anisotropic thin-walled closed-cross-section beams
    • Armanios E.A., and Badir A.M. Free vibration analysis of anisotropic thin-walled closed-cross-section beams. AIAA Journal 33 (1995) 1905-1910
    • (1995) AIAA Journal , vol.33 , pp. 1905-1910
    • Armanios, E.A.1    Badir, A.M.2
  • 2
    • 0027110269 scopus 로고
    • Coupled bending-torsional dynamic stiffness matrix for Timoshenko beam elements
    • Banerjee J.R., and Williams F.W. Coupled bending-torsional dynamic stiffness matrix for Timoshenko beam elements. Computers & Structures 42 (1992) 301-310
    • (1992) Computers & Structures , vol.42 , pp. 301-310
    • Banerjee, J.R.1    Williams, F.W.2
  • 3
    • 0001224924 scopus 로고
    • Free vibration of composite beams - an exact method using symbolic computation
    • Banerjee J.R., and Williams F.W. Free vibration of composite beams - an exact method using symbolic computation. Journal of Aircraft 32 (1995) 636-642
    • (1995) Journal of Aircraft , vol.32 , pp. 636-642
    • Banerjee, J.R.1    Williams, F.W.2
  • 5
    • 85088759910 scopus 로고    scopus 로고
    • T.M. Clements, M. Rais-Rohani, Design optimization of a composite tilt-rotor wing with stability approximations, in: Proc. of 41st AIAA/SME/ASEC/AHS/ASC Structures, Structural Dynamics and Materials Conference, Atlanta, GA, April 2000, pp. 829-838. Paper No. AIAA-2000-1454
  • 6
    • 34249310041 scopus 로고    scopus 로고
    • D.E. Davies, Theoretical determination of subsonic oscillatory airforce coefficients, Royal Aircraft Establishment - Technical Report (RAE-TR-76059), 1978
  • 7
    • 34249288790 scopus 로고    scopus 로고
    • M.A. El-Shinnawey, Ground resonance and normal modes of aerobatic aircraft Cranfield A1, MSc Experimental Thesis, College of Aeronautics, Cranfield University, December 1978
  • 8
    • 0000387235 scopus 로고
    • A rapidly convergent method for minimization
    • Fletcher R., and Powell M.J.D. A rapidly convergent method for minimization. Computer Journal 6 (1963) 163-168
    • (1963) Computer Journal , vol.6 , pp. 163-168
    • Fletcher, R.1    Powell, M.J.D.2
  • 12
    • 28844459466 scopus 로고    scopus 로고
    • S. Guo, W. Chen, D. Cui, Optimization of composite wing structures for maximum flutter speed, in: Proc. of the 1st AIAA Multidisciplinary Design Optimization Specialist Conference, the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Austin, TX, 18-21 April 2005. Paper No. AIAA-2005-2132
  • 13
    • 34249310391 scopus 로고    scopus 로고
    • S. Guo, C.W. Cheung, J.R. Banerjee, R. Butler, Gust alleviation and flutter suppression of an optimized composite wing, in: Proc. of Int. Forum on Aeroelasticity and Structural Dynamics, Manchester, UK, June 1995, pp. 41.1-41.9
  • 15
    • 0021197871 scopus 로고
    • 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 21 (1984) 69-76
    • (1984) Journal of Aircraft , vol.21 , pp. 69-76
    • Hollowell, S.J.1    Dugundji, J.2
  • 18
    • 0024104193 scopus 로고
    • Aeroelastic divergence of swept-forward composite wings including warping restraint effect
    • Librescu L., and Khdeir A.A. Aeroelastic divergence of swept-forward composite wings including warping restraint effect. AIAA Journal 26 (1988) 1373-1377
    • (1988) AIAA Journal , vol.26 , pp. 1373-1377
    • Librescu, L.1    Khdeir, A.A.2
  • 19
    • 0023985604 scopus 로고
    • General formulation for the aeroelastic divergence of composite swept-forward wing structures
    • Librescu L., and Simovich J. General formulation for the aeroelastic divergence of composite swept-forward wing structures. Journal of Aircraft 25 (1988) 364-371
    • (1988) Journal of Aircraft , vol.25 , pp. 364-371
    • Librescu, L.1    Simovich, J.2
  • 20
    • 0026103397 scopus 로고
    • Analytical study on static aeroelastic behavior of swept-forward composite wing structures
    • Librescu L., and Thangjitham S. Analytical study on static aeroelastic behavior of swept-forward composite wing structures. Journal of Aircraft 28 (1991) 151-157
    • (1991) Journal of Aircraft , vol.28 , pp. 151-157
    • Librescu, L.1    Thangjitham, S.2
  • 21
    • 0029213891 scopus 로고    scopus 로고
    • M. Lillico, R. Butler, J.R. Banerjee, S. Guo, Optimum design of high aspect ratio wings subject to aeroelastic constraints, in: Proc. of 36th AIAA/SME/ASEC/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 1995, pp. 558-566
  • 22
    • 0031061903 scopus 로고    scopus 로고
    • Aeroelastic optimization of composite wings using the dynamic stiffness method
    • Lillico M., Butler R., Guo S., and Banerjee J.R. Aeroelastic optimization of composite wings using the dynamic stiffness method. The Aeronautical Journal 101 (1997) 77-86
    • (1997) The Aeronautical Journal , vol.101 , pp. 77-86
    • Lillico, M.1    Butler, R.2    Guo, S.3    Banerjee, J.R.4
  • 23
    • 0022161218 scopus 로고
    • Flutter and divergence aeroelastic characteristics for composite forward swept cantilever wing
    • Lottati I. Flutter and divergence aeroelastic characteristics for composite forward swept cantilever wing. Journal of Aircraft 22 (1985) 1001-1007
    • (1985) Journal of Aircraft , vol.22 , pp. 1001-1007
    • Lottati, I.1
  • 25
    • 0019025136 scopus 로고
    • Divergence of swept-forward composite wings
    • Weisshaar T.A. Divergence of swept-forward composite wings. Journal of Aircraft 17 (1980) 442-448
    • (1980) Journal of Aircraft , vol.17 , pp. 442-448
    • Weisshaar, T.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.