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Volumn 6, Issue , 2004, Pages 4560-4571

Nonlinear aeroelasitic studies on a joined-wing with wing buckling effects

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BUCKLING; COMPUTER SIMULATION; LINEAR SYSTEMS; NONLINEAR SYSTEMS; TIME DOMAIN ANALYSIS; WINGS;

EID: 16244383815     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (9)

References (20)
  • 1
    • 84860102374 scopus 로고
    • "Joined Wing Aircraft," U.S. Patent 3,942,747, March
    • Wolkovitch, J., "Joined Wing Aircraft," U.S. Patent 3,942,747, March 1976.
    • (1976)
    • Wolkovitch, J.1
  • 2
    • 0022680733 scopus 로고
    • The joined wing: An overview
    • Wolkovitch, J., "The Joined Wing: An Overview," Journal of Aircraft, Vol. 23, No. 3, 1986, pp. 161-178.
    • (1986) Journal of Aircraft , vol.23 , Issue.3 , pp. 161-178
    • Wolkovitch, J.1
  • 3
    • 0020139051 scopus 로고
    • Structural weight comparison of a joined wing and a conventional wing
    • Samuels, M. F., "Structural Weight Comparison of a Joined Wing and a Conventional Wing," Journal of Aircraft, Vol. 19, No. 6, 1982, pp. 485-491.
    • (1982) Journal of Aircraft , vol.19 , Issue.6 , pp. 485-491
    • Samuels, M.F.1
  • 4
    • 85088002105 scopus 로고
    • Aerodynamic-structural optimization of positive/negative stagger joined wing configurations
    • AIAA Paper 86-2626, Dayton, Ohio, 20-22, Oct.
    • Selberg, B. P. and Cronin, D. L., "Aerodynamic-Structural Optimization of Positive/Negative Stagger Joined Wing Configurations," AIAA Paper 86-2626, AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting, Dayton, Ohio, 20-22, Oct. 1986.
    • (1986) AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting
    • Selberg, B.P.1    Cronin, D.L.2
  • 5
    • 85088282469 scopus 로고
    • Optimum structural sizing of conventional cantilever and joined-wing configurations using equivalent beam models
    • AIAA Paper 86-2653, Dayton, Ohio, 20-22, Oct.
    • Hajela, P. and Chen, J.L., "Optimum Structural Sizing of Conventional Cantilever and Joined-Wing Configurations Using Equivalent Beam Models," AIAA Paper 86-2653, AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting, Dayton, Ohio, 20-22, Oct. 1986.
    • (1986) AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting
    • Hajela, P.1    Chen, J.L.2
  • 7
    • 0024131041 scopus 로고
    • Parametric weight evaluation of joined wings by structural optimization
    • Miura, H., Shyu, A., and Wolkovitch, J., "Parametric Weight Evaluation of Joined Wings by Structural Optimization," Journal of Aircraft, Vol. 25, No. 12, 1988, pp. 1142-1149.
    • (1988) Journal of Aircraft , vol.25 , Issue.12 , pp. 1142-1149
    • Miura, H.1    Shyu, A.2    Wolkovitch, J.3
  • 10
    • 0027697631 scopus 로고
    • Optimization of joined-wing aircraft
    • Gallman, J. W., Kroo, I. M., and Smith, S. C., "Optimization of Joined-Wing Aircraft," Journal of Aircraft, Vol. 30, No. 4, 1993, pp. 446-452.
    • (1993) Journal of Aircraft , vol.30 , Issue.4 , pp. 446-452
    • Gallman, J.W.1    Kroo, I.M.2    Smith, S.C.3
  • 11
    • 0029710536 scopus 로고    scopus 로고
    • Structural optimization for joined-wing synthesis
    • Jan.-Feb.
    • Gallman, J. W. and Kroo, I. M., "Structural Optimization for Joined-Wing Synthesis," Journal of Aircraft, Vol. 33, No. 1, Jan.-Feb. 1996, pp. 214-223.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 214-223
    • Gallman, J.W.1    Kroo, I.M.2
  • 17
    • 0026257294 scopus 로고
    • Applications of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations
    • Hoadley, S.T. and Karpel, M., "Applications of Aeroservoelastic Modeling Using Minimum-State Unsteady Aerodynamic Approximations," Journal of Guidance, Control and Dynamics, Vol. 14, No. 6, 1991, pp. 1267-1276.
    • (1991) Journal of Guidance, Control and Dynamics , vol.14 , Issue.6 , pp. 1267-1276
    • Hoadley, S.T.1    Karpel, M.2
  • 18
    • 0029341358 scopus 로고
    • Structural dynamic loads in response to impulsive excitation
    • Jul - Aug
    • Karpel, M. and Presente, E., "Structural Dynamic Loads in Response to Impulsive Excitation," Journal of Aircraft, Vol. 32, No. 4, Jul - Aug, 1995. pp. 853-861.
    • (1995) Journal of Aircraft , vol.32 , Issue.4 , pp. 853-861
    • Karpel, M.1    Presente, E.2
  • 19
    • 0027664805 scopus 로고
    • Unsteady subsonic aerodynamics for bodies and wings with external stores including wake effect
    • Sep - Oct
    • Chen, P.C., Lee, H.W. and Liu, D.D., "Unsteady Subsonic Aerodynamics for Bodies and Wings with External Stores Including Wake Effect," Journal of Aircraft, Vol. 30, No. 5, Sep - Oct, 1993, pp. 618-628.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 618-628
    • Chen, P.C.1    Lee, H.W.2    Liu, D.D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.