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Volumn 38, Issue 9, 2000, Pages 1543-1557

Nonlinear response of airfoil section with control surface freeplay to gust loads

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; CHAOS THEORY; DYNAMIC RESPONSE; FLUTTER (AERODYNAMICS); HARMONIC ANALYSIS; MATHEMATICAL MODELS; WIND EFFECTS; WIND TUNNELS;

EID: 0034275338     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1176     Document Type: Article
Times cited : (53)

References (11)
  • 1
    • 0002203305 scopus 로고    scopus 로고
    • Nonlinear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study
    • Conner, M. D., Tang, D. M., Dowell, E. H., and Virgin, L. N., "Nonlinear Behavior of a Typical Airfoil Section with Control Surface Freeplay: A Numerical and Experimental Study," Journal of Fluids and Structures, Vol. 11, No. 1, 1997, pp. 89-109.
    • (1997) Journal of Fluids and Structures , vol.11 , Issue.1 , pp. 89-109
    • Conner, M.D.1    Tang, D.M.2    Dowell, E.H.3    Virgin, L.N.4
  • 2
    • 0018452920 scopus 로고
    • Unsteady aerodynamic modeling for arbitrary motions
    • Edwards, J. W., Ashley, H., and Breakwell, J. V., "Unsteady Aerodynamic Modeling for Arbitrary Motions" AIAA Journal, Vol. 17, No. 4, 1979, pp. 365-374.
    • (1979) AIAA Journal , vol.17 , Issue.4 , pp. 365-374
    • Edwards, J.W.1    Ashley, H.2    Breakwell, J.V.3
  • 4
    • 0032025911 scopus 로고    scopus 로고
    • Reduced-order aerodynamic model and its applications to a nonlinear aeroelastic system
    • Tang, D. M., Conner, M. D., and Dowell, E. H., "Reduced-Order Aerodynamic Model and Its Applications to a Nonlinear Aeroelastic System," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 332-338.
    • (1998) Journal of Aircraft , vol.35 , Issue.2 , pp. 332-338
    • Tang, D.M.1    Conner, M.D.2    Dowell, E.H.3
  • 5
    • 0343855707 scopus 로고    scopus 로고
    • Further physical explanations of free play effects on chaotic flutter response of all-movable control surfaces
    • April
    • Pitt, D. M., "Further Physical Explanations of Free Play Effects on Chaotic Flutter Response of All-Movable Control Surfaces," Second International Conf. on Nonlinear Problems in Aviation and Aerospace, April 1998.
    • (1998) Second International Conf. on Nonlinear Problems in Aviation and Aerospace
    • Pitt, D.M.1
  • 8
    • 0029276936 scopus 로고
    • Finite state induced flow models, part I: Two-dimensional thin airfoil
    • Peters, D. A., and Cao, W. M., "Finite State Induced Flow Models, Part I: Two-Dimensional Thin Airfoil," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 313-322.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 313-322
    • Peters, D.A.1    Cao, W.M.2
  • 9
    • 0029720746 scopus 로고    scopus 로고
    • Experiments and analysis for a gust generator in a wind tunnel
    • Tang, D. M., Cizmas, P. G. A., and Dowell, E. H., "Experiments and Analysis for a Gust Generator in a Wind Tunnel," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 139-148.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 139-148
    • Tang, D.M.1    Cizmas, P.G.A.2    Dowell, E.H.3
  • 10
    • 0033688706 scopus 로고    scopus 로고
    • Control of a three-degree-of-freedom airfoil with limit cycle behavior
    • Clark, R. L., Dowell, E. H., and Frampton, K. D., "Control of a Three-Degree-of-Freedom Airfoil with Limit Cycle Behavior," Journal of Aircraft, Vol. 37, No. 3, 2000, pp. 533-536.
    • (2000) Journal of Aircraft , vol.37 , Issue.3 , pp. 533-536
    • Clark, R.L.1    Dowell, E.H.2    Frampton, K.D.3
  • 11
    • 0032022865 scopus 로고    scopus 로고
    • Experimental active control of a typical section using a trailing edge flap
    • Vipperman, J.S., Clark, R. L., Conner, M., and Dowell, E. H., "Experimental Active Control of a Typical Section Using a Trailing Edge Flap," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 224-229.
    • (1998) Journal of Aircraft , vol.35 , Issue.2 , pp. 224-229
    • Vipperman, J.S.1    Clark, R.L.2    Conner, M.3    Dowell, E.H.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.