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Volumn 39, Issue 5, 2002, Pages 885-888

Limit-cycle hysteresis response for a high-aspect-ratio wing model

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; OSCILLATIONS; WIND TUNNELS;

EID: 0036757612     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3009     Document Type: Article
Times cited : (56)

References (9)
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    • NASA Tn D-7818
    • Hodges, D. H., and Dowell, E. H., "Nonlinear Equations of Motion for the Elastic Bending and Torsion of Twisted Nonuniform Rotor Blades," NASA Tn D-7818, 1974.
    • (1974)
    • Hodges, D.H.1    Dowell, E.H.2
  • 2
    • 0034273845 scopus 로고    scopus 로고
    • Nonlinear aeroelastic analysis of complete aircraft in subsonic flow
    • Patil, M. J., Hodges, D. H., and Cesnik, C. E. S., "Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 753-760.
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  • 3
    • 85036870217 scopus 로고    scopus 로고
    • Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect ratio wings
    • (to be published)
    • Tang, D. M., and Dowell, E. H., "Effects of Geometric Structural Nonlinearity on Flutter and Limit Cycle Oscillations of High-Aspect Ratio Wings," Journal of Fluids and Structures (to be published).
    • Journal of Fluids and Structures
    • Tang, D.M.1    Dowell, E.H.2
  • 4
    • 85087192870 scopus 로고    scopus 로고
    • On the importance of aerodynamic and structural geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings
    • AIAA Paper 2000-1448, April
    • Patil, M. J., and Hodges, D. H., "On the Importance of Aerodynamic and Structural Geometrical Nonlinearities on Aeroelastic Behavior of High-Aspect-Ratio Wings," AIAA Paper 2000-1448, April 2000.
    • (2000)
    • Patil, M.J.1    Hodges, D.H.2
  • 5
    • 0035421036 scopus 로고    scopus 로고
    • Experimental and theoretical study on flutter and limit cycle oscillations of high-aspect-ratio wings
    • Tang, D. M., and Dowell, E. H., "Experimental and Theoretical Study on Flutter and Limit Cycle Oscillations of High-Aspect-Ratio Wings," AIAA Journal, Vol. 39, No. 8, 2001, pp. 1430-1441.
    • (2001) AIAA Journal , vol.39 , Issue.8 , pp. 1430-1441
    • Tang, D.M.1    Dowell, E.H.2
  • 6
    • 0036493461 scopus 로고    scopus 로고
    • Experimental and theoretical study of gust response for a high-aspect-ratio wing
    • Tang, D. M., and Dowell, E. H., "Experimental and Theoretical Study of Gust Response for a High-Aspect-Ratio Wing," AIAA Journal, Vol. 40, No. 3, 2002, pp. 419-429.
    • (2002) AIAA Journal , vol.40 , Issue.3 , pp. 419-429
    • Tang, D.M.1    Dowell, E.H.2
  • 7
    • 0019681685 scopus 로고
    • Semi-empirical model for the dynamic stall of airfoils in view to the application to the calculation of responses of a helicopter blade in forward flight
    • Tran, C. T., and Petot, D., "Semi-Empirical Model for the Dynamic Stall of Airfoils in View to the Application to the Calculation of Responses of a Helicopter Blade in Forward Flight," Vertica, Vol. 5, No. 1, 1981, pp. 35-53.
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    • Tran, C.T.1    Petot, D.2
  • 8
    • 0026617158 scopus 로고
    • Nonlinear stall flutter and divergence analysis of cantilevered graphite/epoxy wings
    • Dunn, P., and Dugundji, J., "Nonlinear Stall Flutter and Divergence Analysis of Cantilevered Graphite/Epoxy Wings," AIAA Journal, Vol. 30, No. 1, 1992, pp. 153-162.
    • (1992) AIAA Journal , vol.30 , Issue.1 , pp. 153-162
    • Dunn, P.1    Dugundji, J.2
  • 9
    • 0027642269 scopus 로고
    • Nonlinear large amplitude aeroelastic behavior of composite rotor blades
    • Kim, T., and Dugundji, J., "Nonlinear Large Amplitude Aeroelastic Behavior of Composite Rotor Blades," AIAA Journal, Vol. 31, No. 8, 1993, pp. 1489-1497.
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    • Kim, T.1    Dugundji, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.