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Volumn , Issue , 2008, Pages

Coupled nonlinear aeroelastic and aeroacoustic response of an airfoil to upstream vortical flow disturbances

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AERODYNAMICS; AEROELASTICITY; AIRFOILS; CONTROL NONLINEARITIES; EQUATIONS OF MOTION; NONLINEAR EQUATIONS;

EID: 78249250314     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-3047     Document Type: Conference Paper
Times cited : (1)

References (35)
  • 2
    • 84959324234 scopus 로고    scopus 로고
    • An overview of recent developments in computational aeroelasticity
    • Bennett, R. and Edwards, J., (1998) "An Overview of Recent Developments in Computational Aeroelasticity," AIAA Paper 98-2421.
    • (1998) AIAA Paper 98-2421
    • Bennett, R.1    Edwards, J.2
  • 3
    • 0011453930 scopus 로고    scopus 로고
    • Reduced-order modeling: New approaches for computational physics
    • Beran, P. and Silva, W, (2001) "Reduced-Order Modeling: New Approaches for Computational Physics," AIAA Paper 2001-0853.
    • (2001) AIAA Paper 2001-0853
    • Beran, P.1    Silva, W.2
  • 4
    • 0034273845 scopus 로고    scopus 로고
    • Nonlinear aeroelastic analysis of complete aircraft in subsonic flow
    • Patil, M., Hodges, D. and Cesnik, C., (2000) "Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow," Journal of Aircraft, Vol.37, No.5, pp. 753-760.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 753-760
    • Patil, M.1    Hodges, D.2    Cesnik, C.3
  • 6
    • 0035527295 scopus 로고    scopus 로고
    • Limit-cycle oscillations in high-aspect-ratio wings
    • Patil, M., Hodges, D. and Cesnik, C., (2001) "Limit-Cycle Oscillations in High-Aspect-Ratio Wings," Journal of Fluids and Structures, Vol. 15, pp. 107-132.
    • (2001) Journal of Fluids and Structures , vol.15 , pp. 107-132
    • Patil, M.1    Hodges, D.2    Cesnik, C.3
  • 7
    • 33646394613 scopus 로고    scopus 로고
    • Flutter and limit-cycle oscillation for a wing-store model with freeplay
    • Tang, D. and Dowell, E., (2006) "Flutter and Limit-Cycle Oscillation for a Wing-Store Model with Freeplay," Journal of Aircraft, Vol.43, No.2, pp.387-503.
    • (2006) Journal of Aircraft , vol.43 , Issue.2 , pp. 387-503
    • Tang, D.1    Dowell, E.2
  • 8
    • 0035272350 scopus 로고    scopus 로고
    • Navier-stokes computations of limit-cycle oscillations for a B-1-like configuration
    • 2001
    • Hartwich, P., Dobbs, S., Arslan, A. and Kim, S., (2001) "Navier-Stokes Computations of Limit-Cycle Oscillations for a B-1-Like Configuration," Journal of Aircraft, Vol.38, No.2, 2001.
    • (2001) Journal of Aircraft , vol.38 , Issue.2
    • Hartwich, P.1    Dobbs, S.2    Arslan, A.3    Kim, S.4
  • 10
    • 0025431502 scopus 로고
    • Numerical model of unsteady subsonic aeroelastic behavior
    • Strganac, T. and Mook, D., (1990) "Numerical Model of Unsteady Subsonic Aeroelastic Behavior," AIAA Journal, Vol. 28, No.5, pp. 903-909.
    • (1990) AIAA Journal , vol.28 , Issue.5 , pp. 903-909
    • Strganac, T.1    Mook, D.2
  • 11
    • 0031676451 scopus 로고    scopus 로고
    • On the presence of internal resonances in aeroelastic systems
    • Gilliat, H., Strganac, T., and Kurdila, A., (1998) "On the Presence of Internal Resonances in Aeroelastic Systems," AIAA Paper 98-1954.
    • (1998) AIAA Paper 98-1954
    • Gilliat, H.1    Strganac, T.2    Kurdila, A.3
  • 13
    • 0034316194 scopus 로고    scopus 로고
    • Identification and control of limit cycle oscillations in aeroelastic systems
    • Strganac, T., Ko, J. and Thompson, D., (2000) "Identification and Control of Limit Cycle Oscillations in Aeroelastic Systems," Journal of Guidance, Control, and Dynamics, Vol. 23, No.6, pp. 1127-1133.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.6 , pp. 1127-1133
    • Strganac, T.1    Ko, J.2    Thompson, D.3
  • 14
    • 0032114616 scopus 로고    scopus 로고
    • Aeroelastic response of a rigid wing supported by nonlinear springs
    • O'Neil, T. and Strganac, T., (1998) "Aeroelastic Response of a Rigid Wing Supported by Nonlinear Springs," Journal of Aircraft, Vol. 35, No.4, pp. 616-622.
    • (1998) Journal of Aircraft , vol.35 , Issue.4 , pp. 616-622
    • O'neil, T.1    Strganac, T.2
  • 15
    • 0036531499 scopus 로고    scopus 로고
    • Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations
    • Thomas, J., Dowell, E. and Hall, K., (2002) "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations," AIAA Journal, Vol.40, No.4, pp.638-646.
    • (2002) AIAA Journal , vol.40 , Issue.4 , pp. 638-646
    • Thomas, J.1    Dowell, E.2    Hall, K.3
  • 16
    • 0042513866 scopus 로고    scopus 로고
    • Modeling limit cycle oscillations for an NLR7301 airfoil aeroelastic configuration including correlation with experiment
    • Thomas, J., Dowell, E. and Hall, K, (2003) "Modeling Limit Cycle Oscillations for an NLR7301 Airfoil Aeroelastic Configuration Including Correlation with Experiment," AIAA Paper 2003-1429.
    • (2003) AIAA Paper 2003-1429
    • Thomas, J.1    Dowell, E.2    Hall, K.3
  • 17
    • 0012535159 scopus 로고    scopus 로고
    • The state-of-the-art of unsteady aerodynamics for high performance aircraft
    • Yurkovich, R., Liu, D. and Chen, P., (2001) "The State-of-the-Art of Unsteady Aerodynamics for High Performance Aircraft," AIAA Paper 2001-0428.
    • (2001) AIAA Paper 2001-0428
    • Yurkovich, R.1    Liu, D.2    Chen, P.3
  • 18
    • 0035006811 scopus 로고    scopus 로고
    • An optimal reduced-order aeroelastic modeling based on a response-based modal analysis of unsteady CFD models
    • Kim, T. and Bussoletti, J., (2001) "An Optimal Reduced-Order Aeroelastic Modeling Based on a Response-Based Modal Analysis of Unsteady CFD Models," AIAA Paper 2001-1525.
    • (2001) AIAA Paper 2001-1525
    • Kim, T.1    Bussoletti, J.2
  • 19
    • 0042127417 scopus 로고    scopus 로고
    • Aircraft aeroelastic analysis and design using CFD based unsteady loads
    • Raveh, D., Levy, Y. and Karpel, M., (2000) "Aircraft Aeroelastic Analysis and Design Using CFDbased Unsteady Loads," AIAA Paper 2000-1325.
    • (2000) AIAA Paper 2000-1325
    • Raveh, D.1    Levy, Y.2    Karpel, M.3
  • 20
    • 0007689333 scopus 로고
    • Transonic flutter analysis using the euler equations
    • Bendiksen, O. and Kousen, K., (1987) "Transonic Flutter Analysis Using the Euler Equations," AIAA Paper 87-0911.
    • (1987) AIAA Paper 87-0911
    • Bendiksen, O.1    Kousen, K.2
  • 21
    • 0025249138 scopus 로고
    • Aeroelastic analysis of wings using the euler equations with a deforming mesh
    • Robinson, B., Batina, J., and Yang, H., (1990) "Aeroelastic Analysis of Wings Using the Euler Equations with a Deforming Mesh," AIAA Paper 90-1032.
    • (1990) AIAA Paper 90-1032
    • Robinson, B.1    Batina, J.2    Yang, H.3
  • 22
    • 85067319932 scopus 로고    scopus 로고
    • CFD-based analysis of nonlinear aeroelastic behavior of high-aspect ratio wings
    • Smith, M., Patil, M., and Hodges, D., (2001) "CFD-Based Analysis of Nonlinear Aeroelastic Behavior of High-Aspect Ratio Wings," AIAA Paper 2001-1582.
    • (2001) AIAA Paper 2001-1582
    • Smith, M.1    Patil, M.2    Hodges, D.3
  • 24
    • 34547505701 scopus 로고    scopus 로고
    • Nonlinear gust response of highly flexible aircraft
    • Patil, M., (2007) "Nonlinear Gust Response of Highly Flexible Aircraft," AIAA Paper 2007-2103.
    • (2007) AIAA Paper 2007-2103
    • Patil, M.1
  • 25
    • 0347603505 scopus 로고    scopus 로고
    • Investigation of limit cycle oscillations for a wing section with nonlinear stiffness
    • Berggren, D., (2004) "Investigation of Limit Cycle Oscillations for a Wing Section with Nonlinear Stiffness," Aerospace Science and Technology, Vol.8, pp. 27-34.
    • (2004) Aerospace Science and Technology , vol.8 , pp. 27-34
    • Berggren, D.1
  • 27
    • 19944392926 scopus 로고    scopus 로고
    • Numerical inviscid analysis of nonlinear airfoil response to impinging high-intensity high-frequency gust
    • Golubev, V.V., Mankbadi, R.R. and Scott, J.R., (2004) "Numerical Inviscid Analysis of Nonlinear Airfoil Response to Impinging High-Intensity High-Frequency Gust," AIAA Paper 2004-3002.
    • (2004) AIAA Paper 2004-3002
    • Golubev, V.V.1    Mankbadi, R.R.2    Scott, J.R.3
  • 29
    • 33645152554 scopus 로고    scopus 로고
    • Application of a nonlinear computational aeroacoustics code to the gust-airfoil problem
    • Hixon, R., Golubev, V.V., Mankbadi, R.R., Scott, J.R., Sawyer, S. and Nallasamy, M., (2006) "Application of a Nonlinear Computational Aeroacoustics Code to the Gust-Airfoil Problem," AIAA Journal, Vol. 44, No.2, pp. 323-328.
    • (2006) AIAA Journal , vol.44 , Issue.2 , pp. 323-328
    • Hixon, R.1    Golubev, V.V.2    Mankbadi, R.R.3    Scott, J.R.4    Sawyer, S.5    Nallasamy, M.6
  • 31
    • 84884732752 scopus 로고    scopus 로고
    • Numerical simulation of unsteady response of an oscillating airfoil subject to a high-intensity gust
    • Golubev, V.V., Mankbadi, R.R., Visbal, M.R. and Hixon, R. (2007) "Numerical Simulation of Unsteady Response of an Oscillating Airfoil Subject to a High-Intensity Gust," AIAA Paper 2007-3513.
    • (2007) AIAA Paper 2007-3513
    • Golubev, V.V.1    Mankbadi, R.R.2    Visbal, M.R.3    Hixon, R.4
  • 32
    • 78149421428 scopus 로고    scopus 로고
    • Investigations of nonlinear unsteady aerodynamic and aeroacoustic responses of oscillating airfoils in non-uniform flow
    • Golubev, V.V., Houston, M.J., Golubev, N.V., and Visbal, M.R., (2008) "Investigations of Nonlinear Unsteady Aerodynamic and Aeroacoustic Responses of Oscillating Airfoils in Non-Uniform Flow," AIAA Paper 2008-0033.
    • (2008) AIAA Paper 2008-0033
    • Golubev, V.V.1    Houston, M.J.2    Golubev, N.V.3    Visbal, M.R.4
  • 35
    • 78149433830 scopus 로고    scopus 로고
    • High-accuracy moving wall boundary conditions for computational aeroacoustics
    • Hixon, R., (2008) "High-Accuracy Moving Wall Boundary Conditions for Computational Aeroacoustics," AIAA Paper 2008-30.
    • (2008) AIAA Paper 2008-30
    • Hixon, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.