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Volumn 2012, Issue , 2012, Pages

Support-vector-machine-based reduced-order model for limit cycle oscillation prediction of nonlinear aeroelastic system

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC EFFECTS; AEROELASTIC SYSTEM; EIGEN MODES; FLIGHT SIMULATION; FLOW PARAMETERS; LIMIT CYCLE OSCILLATION (LCO); NONLINEAR AEROELASTIC SYSTEM; NONLINEAR UNSTEADY AERODYNAMICS; REDUCED ORDER MODELS;

EID: 84863241349     PISSN: 1024123X     EISSN: 15635147     Source Type: Journal    
DOI: 10.1155/2012/152123     Document Type: Article
Times cited : (39)

References (32)
  • 1
    • 1342283898 scopus 로고    scopus 로고
    • Reduced-order modeling: New approaches for computational physics
    • Lucia D. J., Beran P. S., Silva W. A., Reduced-order modeling: new approaches for computational physics Progress in Aerospace Sciences 2004 40 1-2 51 117
    • (2004) Progress in Aerospace Sciences , vol.40 , Issue.12 , pp. 51-117
    • Lucia, D.J.1    Beran, P.S.2    Silva, W.A.3
  • 2
    • 3042826212 scopus 로고    scopus 로고
    • Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code
    • DOI 10.1016/j.jfluidstructs.2004.03.004, PII S088997460400057X
    • Silva W. A., Bartels R. E., Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code Journal of Fluids and Structures 2004 19 6 729 745 (Pubitemid 38870837)
    • (2004) Journal of Fluids and Structures , vol.19 , Issue.6 , pp. 729-745
    • Silva, W.A.1    Bartels, R.E.2
  • 4
    • 0034298665 scopus 로고    scopus 로고
    • Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows
    • Hall K. C., Thomas J. P., Dowell E. H., Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows AIAA Journal 2000 38 10 1853 1862
    • (2000) AIAA Journal , vol.38 , Issue.10 , pp. 1853-1862
    • Hall, K.C.1    Thomas, J.P.2    Dowell, E.H.3
  • 5
    • 70350365921 scopus 로고    scopus 로고
    • A fast aeroelastic response prediction method based on proper orthogonal decomposition reduced order model
    • Chen G., Li Y.-M., Yan G.-R., Xu M., Zeng X.-A., A fast aeroelastic response prediction method based on proper orthogonal decomposition reduced order model Journal of Astronautics 2009 30 5 1765 1769
    • (2009) Journal of Astronautics , vol.30 , Issue.5 , pp. 1765-1769
    • Chen, G.1    Li, Y.-M.2    Yan, G.-R.3    Xu, M.4    Zeng, X.-A.5
  • 6
    • 34347252618 scopus 로고    scopus 로고
    • Fast prediction of transonic aeroelastic stability and limit cycles
    • DOI 10.2514/1.25604
    • Badcock K. J., Woodgate M. A., Fast prediction of transonic aeroelastic stability and limit cycles AIAA Journal 2007 45 6 1370 1381 (Pubitemid 46997902)
    • (2007) AIAA Journal , vol.45 , Issue.6 , pp. 1370-1381
    • Woodgate, M.A.1    Badcock, K.J.2
  • 7
    • 77049124832 scopus 로고    scopus 로고
    • Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver
    • Thomas J. P., Dowell E. H., Hall K. C., Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver AIAA Journal 2010 48 1 19 24
    • (2010) AIAA Journal , vol.48 , Issue.1 , pp. 19-24
    • Thomas, J.P.1    Dowell, E.H.2    Hall, K.C.3
  • 8
    • 80051789180 scopus 로고    scopus 로고
    • Transonic aeroelastic simulation for instability searchesand uncertainty analysis
    • Badcock K. J., Timme S., Marques S., Transonic aeroelastic simulation for instability searchesand uncertainty analysis Progress in Aerospace Sciences 2011 47 392 423
    • (2011) Progress in Aerospace Sciences , vol.47 , pp. 392-423
    • Badcock, K.J.1    Timme, S.2    Marques, S.3
  • 9
    • 77955519257 scopus 로고    scopus 로고
    • A nonlinear POD reduced order model for limit cycle oscillation prediction
    • Chen G., Li Y., Yan G., A nonlinear POD reduced order model for limit cycle oscillation prediction Science China 2010 53 7 1325 1332
    • (2010) Science China , vol.53 , Issue.7 , pp. 1325-1332
    • Chen, G.1    Li, Y.2    Yan, G.3
  • 10
    • 79952612345 scopus 로고    scopus 로고
    • Limit cycle oscillation prediction and control design method for aeroelastic system based on new nonlinear reduced order model
    • Chen G., Li Y.-M., Yan G.-R., Limit cycle oscillation prediction and control design method for aeroelastic system based on new nonlinear reduced order model International Journal of Computational Methods 2011 8 1 77 90
    • (2011) International Journal of Computational Methods , vol.8 , Issue.1 , pp. 77-90
    • Chen, G.1    Li, Y.-M.2    Yan, G.-R.3
  • 11
    • 3042795181 scopus 로고    scopus 로고
    • Identification of computational-fluid-dynamics based unsteady aerodynamic models for aeroelastic analysis
    • Raveh D. E., Identification of computational-fluid-dynamics based unsteady aerodynamic models for aeroelastic analysis Journal of Aircraft 2004 41 3 620 632
    • (2004) Journal of Aircraft , vol.41 , Issue.3 , pp. 620-632
    • Raveh, D.E.1
  • 12
    • 49349091754 scopus 로고    scopus 로고
    • Simultaneous excitation of multiple-input/multiple-output CFD-based unsteady aerodynamic systems
    • Silva W. A., Simultaneous excitation of multiple-input/multiple-output CFD-based unsteady aerodynamic systems Journal of Aircraft 2008 45 4 1267 1274
    • (2008) Journal of Aircraft , vol.45 , Issue.4 , pp. 1267-1274
    • Silva, W.A.1
  • 13
    • 0035527291 scopus 로고    scopus 로고
    • Identification and prediction of unsteady transonic aerodynamic loads by multi-layer functionals
    • DOI 10.1006/jfls.2000.0321
    • Marques F. D., Anderson J., Identification and prediction of unsteady transonic aerodynamic loads by multi-layer functionals Journal of Fluids and Structures 2001 15 1 83 106 (Pubitemid 32337819)
    • (2001) Journal of Fluids and Structures , vol.15 , Issue.1 , pp. 83-106
    • Marques, F.D.1    Anderson, J.2
  • 14
    • 34147210049 scopus 로고    scopus 로고
    • Flutter simulation and prediction with CFD-based reduced-order model
    • AIAA 2006-2026, Collection of Technical Papers - 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference: 14th AIAA/ASME/AHS Adaptive Structures Conference, 8th AIAA Non-deterministic App
    • Lai K. L., Won K. S., Koh E. P. C., Tsai H. M., Flutter simulation and prediction with CFD-based reduced-order model Proceedings of the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (AIAA '06) May 2006 Newport, RI, USA 5229 5245 (Pubitemid 46581652)
    • (2006) Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference , vol.7 , pp. 5229-5245
    • Lai, K.L.1    Won, K.S.2    Koh, E.P.C.3    Tsai, H.M.4
  • 15
    • 33750906227 scopus 로고    scopus 로고
    • Identification of nonlinear systems using wavelets and neural network
    • 5-A
    • Srivastava S., Singh M., Hanmandlu M., Jha A. N., Identification of nonlinear systems using wavelets and neural network IETE Journal of Research 2006 52 4 305 313 (Pubitemid 44726297)
    • (2006) IETE Journal of Research , vol.52 , Issue.4 , pp. 305-313
    • Srivastava, S.1    Singh, M.2    Hanmandlu, M.3    Jha, A.N.4
  • 16
  • 19
    • 0032594959 scopus 로고    scopus 로고
    • An overview of statistical learning theory
    • Vapnik V. N., An overview of statistical learning theory IEEE Transactions on Neural Networks 1999 10 5 988 999
    • (1999) IEEE Transactions on Neural Networks , vol.10 , Issue.5 , pp. 988-999
    • Vapnik, V.N.1
  • 20
    • 27644524925 scopus 로고    scopus 로고
    • Subspace identification of Hammerstein systems using least squares support vector machines
    • DOI 10.1109/TAC.2005.856647
    • Goethals I., Pelckmans K., Suykens J. A. K., De Moor B., Subspace identification of Hammerstein systems using least squares support vector machines IEEE Transactions on Automatic Control 2005 50 10 1509 1519 (Pubitemid 41555601)
    • (2005) IEEE Transactions on Automatic Control , vol.50 , Issue.10 , pp. 1509-1519
    • Goethals, I.1    Pelckmans, K.2    Suykens, J.A.K.3    De Moor, B.4
  • 21
    • 53749102436 scopus 로고    scopus 로고
    • Non-Mercer hybrid kernel for linear programming support vector regression in nonlinear systems identification
    • Lu Z., Sun J., Non-Mercer hybrid kernel for linear programming support vector regression in nonlinear systems identification Applied Soft Computing Journal 2009 9 1 94 99
    • (2009) Applied Soft Computing Journal , vol.9 , Issue.1 , pp. 94-99
    • Lu, Z.1    Sun, J.2
  • 25
    • 70350714263 scopus 로고    scopus 로고
    • Weighted solution path algorithm of support vector regression based on heuristic weight-setting optimization
    • Mao W., Yan G., Dong L., Weighted solution path algorithm of support vector regression based on heuristic weight-setting optimization Neurocomputing 2009 73 13 495 505
    • (2009) Neurocomputing , vol.73 , Issue.13 , pp. 495-505
    • Mao, W.1    Yan, G.2    Dong, L.3
  • 26
    • 15344349684 scopus 로고    scopus 로고
    • Fluid-structure interaction for aeroelastic applications
    • DOI 10.1016/j.paerosci.2005.01.001, PII S0376042105000084
    • Kamakoti R., Shyy W., Fluid-structure interaction for aeroelastic applications Progress in Aerospace Sciences 2004 40 8 535 558 (Pubitemid 40391501)
    • (2004) Progress in Aerospace Sciences , vol.40 , Issue.8 , pp. 535-558
    • Kamakoti, R.1    Shyy, W.2
  • 27
    • 0036531499 scopus 로고    scopus 로고
    • Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations
    • Thomas J. P., Dowell E. H., Hall K. C., Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations AIAA Journal 2002 40 4 638 646 (Pubitemid 34555101)
    • (2002) AIAA Journal , vol.40 , Issue.4 , pp. 638-646
    • Thomas, J.P.1    Dowell, E.H.2    Hall, K.C.3
  • 30
    • 47749108243 scopus 로고    scopus 로고
    • Interpolation method for adapting reduced-order models and application to aeroelasticity
    • Amsallem D., Farhat C., Interpolation method for adapting reduced-order models and application to aeroelasticity AIAA Journal 2008 46 7 1803 1813
    • (2008) AIAA Journal , vol.46 , Issue.7 , pp. 1803-1813
    • Amsallem, D.1    Farhat, C.2
  • 31
    • 77957173096 scopus 로고    scopus 로고
    • Toward real-time computational-fluid-dynamics-based aeroelastic computations using a database of reduced-order information
    • Amsallem D., Cortial J., Farhat C., Toward real-time computational-fluid- dynamics-based aeroelastic computations using a database of reduced-order information AIAA Journal 2010 48 9 2029 2037
    • (2010) AIAA Journal , vol.48 , Issue.9 , pp. 2029-2037
    • Amsallem, D.1    Cortial, J.2    Farhat, C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.