메뉴 건너뛰기




Volumn 27, Issue 8, 2011, Pages 1447-1454

Equivalent damping of aeroelastic system of an airfoil with cubic stiffness

Author keywords

Aerodynamics; Equivalent damping; Nonlinear aeroelastics

Indexed keywords

AEROELASTIC SYSTEM; CUBIC STIFFNESS; EQUIVALENT DAMPING; EQUIVALENT SYSTEM; HARMONIC BALANCE METHOD; MATHEMATICAL TREATMENTS; NONLINEAR AEROELASTICS; NUMERICAL EXAMPLE; NUMERICAL INTEGRATION METHODS; PITCH STIFFNESS; UNSTEADY AERODYNAMICS;

EID: 80053052562     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2011.02.004     Document Type: Article
Times cited : (19)

References (13)
  • 1
    • 57349128447 scopus 로고    scopus 로고
    • Bifurcation analysis of a two-degree-of-freedom aeroelastic system with hysteresis structural nonlinearity by a perturbation-incremental method
    • Chung K.W., He Y.B., Lee B.H.K. Bifurcation analysis of a two-degree-of-freedom aeroelastic system with hysteresis structural nonlinearity by a perturbation-incremental method. Journal of Sound and Vibration 2009, 320:163-183.
    • (2009) Journal of Sound and Vibration , vol.320 , pp. 163-183
    • Chung, K.W.1    He, Y.B.2    Lee, B.H.K.3
  • 3
    • 70149114149 scopus 로고    scopus 로고
    • True damping and frequency prediction for aeroelastic systems: the PP method
    • Haddadpour H., Firouz-Abadi R.D. True damping and frequency prediction for aeroelastic systems: the PP method. Journal of Fluids and Structures 2009, 25(7):1177-1188.
    • (2009) Journal of Fluids and Structures , vol.25 , Issue.7 , pp. 1177-1188
    • Haddadpour, H.1    Firouz-Abadi, R.D.2
  • 4
    • 0004024098 scopus 로고
    • The unsteady lift of a wing of finite aspect ratio.
    • NACA Report 681.
    • Jones, R.T., 1940. The unsteady lift of a wing of finite aspect ratio. NACA Report 681.
    • (1940)
    • Jones, R.T.1
  • 5
    • 0001138577 scopus 로고    scopus 로고
    • Analysis and computation of nonlinear dynamic response of a two-degree-of-freedom system and its application in aeroelasticity
    • Lee B.H.K., Gong L., Wong Y.S. Analysis and computation of nonlinear dynamic response of a two-degree-of-freedom system and its application in aeroelasticity. Journal of Fluids and Structures 1997, 11:225-246.
    • (1997) Journal of Fluids and Structures , vol.11 , pp. 225-246
    • Lee, B.H.K.1    Gong, L.2    Wong, Y.S.3
  • 6
    • 0033115309 scopus 로고    scopus 로고
    • Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos
    • Lee B.H.K., Price S.J., Wong Y.S. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos. Progress in Aerospace Science 1999, 35:205-344.
    • (1999) Progress in Aerospace Science , vol.35 , pp. 205-344
    • Lee, B.H.K.1    Price, S.J.2    Wong, Y.S.3
  • 7
    • 13444274398 scopus 로고    scopus 로고
    • Airfoil motion in subsonic flow with strong cubic nonlinear restoring forces
    • Lee B.H.K., Liu L.P., Chung K.W. Airfoil motion in subsonic flow with strong cubic nonlinear restoring forces. Journal of Sound and Vibration 2005, 281:699-717.
    • (2005) Journal of Sound and Vibration , vol.281 , pp. 699-717
    • Lee, B.H.K.1    Liu, L.P.2    Chung, K.W.3
  • 8
    • 0034224760 scopus 로고    scopus 로고
    • Application of the center manifold theory in nonlinear aeroelasticity
    • Liu L.P., Wong Y.S., Lee B.H.K. Application of the center manifold theory in nonlinear aeroelasticity. Journal of Sound and Vibration 2000, 234:641-659.
    • (2000) Journal of Sound and Vibration , vol.234 , pp. 641-659
    • Liu, L.P.1    Wong, Y.S.2    Lee, B.H.K.3
  • 9
    • 4444319322 scopus 로고    scopus 로고
    • The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics
    • Liu L.P., Dowell E.H. The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics. Nonlinear Dynamics 2004, 37:31-49.
    • (2004) Nonlinear Dynamics , vol.37 , pp. 31-49
    • Liu, L.P.1    Dowell, E.H.2
  • 10
    • 34047163427 scopus 로고    scopus 로고
    • A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces
    • Liu L.P., Dowell E.H., Thomas J.P. A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces. Journal of Fluids and Structures 2007, 23:351-363.
    • (2007) Journal of Fluids and Structures , vol.23 , pp. 351-363
    • Liu, L.P.1    Dowell, E.H.2    Thomas, J.P.3
  • 11
    • 77955656738 scopus 로고    scopus 로고
    • Assessment of added mass effects on flutter boundaries using the Leishman-Beddoes dynamic stall model
    • Peiro J., Galvanetto U., Chantharasenawong C. Assessment of added mass effects on flutter boundaries using the Leishman-Beddoes dynamic stall model. Journal of Fluids and Structures 2010, 26(5):814-840.
    • (2010) Journal of Fluids and Structures , vol.26 , Issue.5 , pp. 814-840
    • Peiro, J.1    Galvanetto, U.2    Chantharasenawong, C.3
  • 12
    • 0037068913 scopus 로고    scopus 로고
    • Limit cycle flutter of airfoils in steady and unsteady flows
    • Shahrzad P., Mahzoon M. Limit cycle flutter of airfoils in steady and unsteady flows. Journal of Sound and Vibration 2002, 256(2):213-225.
    • (2002) Journal of Sound and Vibration , vol.256 , Issue.2 , pp. 213-225
    • Shahrzad, P.1    Mahzoon, M.2
  • 13
    • 60649094522 scopus 로고    scopus 로고
    • Stability of a two-dimensional airfoil with time-delayed feedback control
    • Zhao Y.H. Stability of a two-dimensional airfoil with time-delayed feedback control. Journal of Fluids and Structures 2009, 25(1):1-25.
    • (2009) Journal of Fluids and Structures , vol.25 , Issue.1 , pp. 1-25
    • Zhao, Y.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.