메뉴 건너뛰기




Volumn , Issue , 2005, Pages 8827-8843

Flutter simulation and prediction via identification of non-linear impulse response

Author keywords

[No Author keywords available]

Indexed keywords

AUTOREGRESSIVE MOVING; FLUTTER SIMULATION; MULTISTEP FUNCTION METHOD;

EID: 30744471154     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (31)
  • 1
    • 0017932980 scopus 로고
    • Computation of unsteady transonic flows by the indicia! method
    • February
    • Ballhaus, W.F. and Goorjian, P.M. Computation of Unsteady Transonic Flows by the Indicia! Method. AIAA Journal, pp. 117-124, February 1978.
    • (1978) AIAA Journal , pp. 117-124
    • Ballhaus, W.F.1    Goorjian, P.M.2
  • 2
    • 0023435191 scopus 로고
    • Transonic aeroelasticity of wings with tip stores
    • Oct.
    • Guruswamy, G.P., Goorjian, P.M., and Tu, E.L. Transonic Aeroelasticity of Wings with Tip Stores. Journal of Aircraft, Vol. 24, No. 10, pp. 688-695, Oct. 1987.
    • (1987) Journal of Aircraft , vol.24 , Issue.10 , pp. 688-695
    • Guruswamy, G.P.1    Goorjian, P.M.2    Tu, E.L.3
  • 3
    • 0024091362 scopus 로고
    • Unsteady transonic aerodynamics and aeroelastic calculations at low-supersonic freestreams
    • Oct.
    • Guruswamy, G.P. and Goorjian, P.M. Unsteady Transonic Aerodynamics and Aeroelastic Calculations at Low-Supersonic Freestreams. Journal of Aircraft, Vol. 25, No. 10, pp. 955-961, Oct. 1988.
    • (1988) Journal of Aircraft , vol.25 , Issue.10 , pp. 955-961
    • Guruswamy, G.P.1    Goorjian, P.M.2
  • 4
    • 0029277237 scopus 로고
    • Wing flutter boundary prediction using unsteady Euler aerodynamic method
    • March-April
    • Lee-Rausch, E.M. and Batina, J.T. Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method. Journal of Aircraft, Vol. 32, No. 2, pp. 416-422, March-April 1995.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 416-422
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 5
    • 0026261105 scopus 로고
    • Aeroelastic analysis of wings using the Euler equation with a deforming mesh
    • November
    • Robinson, B.A., Batina, J.T., and Yang, H.T.Y. Aeroelastic Analysis of Wings Using the Euler Equation with a Deforming Mesh. Journal of Aircraft, Vol. 28, No. 11, pp. 781-788, November 1991.
    • (1991) Journal of Aircraft , vol.28 , Issue.11 , pp. 781-788
    • Robinson, B.A.1    Batina, J.T.2    Yang, H.T.Y.3
  • 6
    • 0035272355 scopus 로고    scopus 로고
    • Calculation of wing flutter by a coupled fluid-structure method
    • March-April
    • Liu, F., Cai, J., Zhu, Y., Tsai, H.M., and Wong, A.S.F. Calculation of Wing Flutter by a Coupled Fluid-Structure Method. Journal of Aircraft, Vol. 38, pp. 334-342, March-April 2001.
    • (2001) Journal of Aircraft , vol.38 , pp. 334-342
    • Liu, F.1    Cai, J.2    Zhu, Y.3    Tsai, H.M.4    Wong, A.S.F.5
  • 7
    • 2942706766 scopus 로고    scopus 로고
    • Parallel computation of wing flutter with a coupled Navier-Stoke/CSD method
    • Jan.
    • Sadeghi, M., Yang, S., Liu, F., and Tsai, H.M. Parallel Computation of Wing Flutter with a Coupled Navier-Stoke/CSD Method. AIAA Paper-2003-1347, Jan. 2003.
    • (2003) AIAA Paper-2003-1347
    • Sadeghi, M.1    Yang, S.2    Liu, F.3    Tsai, H.M.4
  • 8
    • 84982319130 scopus 로고    scopus 로고
    • Reduced-order modeling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique
    • AIAA Paper-99-0655. 37th, Reno, Nev
    • Hall, K.C., Thomas, J.P. and Dowell, E.H. Reduced-Order Modeling of Unsteady Small-disturbance Flows using a Frequency-domain Proper Orthogonal Decomposition Technique. AIAA Paper-99-0655. Presented at AIAA Aerosp. Sci. Meeting and Exhib., 37th, Reno, Nev, 1999.
    • (1999) AIAA Aerosp. Sci. Meeting and Exhib.
    • Hall, K.C.1    Thomas, J.P.2    Dowell, E.H.3
  • 9
    • 0034965813 scopus 로고    scopus 로고
    • Modeling of fluid-structure interaction
    • Jan
    • Dowell, E.H. and Hall, K.C. Modeling of Fluid-Structure Interaction. Annual Review of Fluid Mechanics, Vol. 33, pp. 445-490, Jan 2001.
    • (2001) Annual Review of Fluid Mechanics , vol.33 , pp. 445-490
    • Dowell, E.H.1    Hall, K.C.2
  • 11
    • 0027664172 scopus 로고
    • Application of non-linear systems theory to transonic unsteady aerodynamic responses
    • Silva, W.A. Application of Non-linear Systems Theory to Transonic Unsteady Aerodynamic Responses. Journal of Aircraft, Vol. 30, No. 5, pp. 660-680, 1993.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 660-680
    • Silva, W.A.1
  • 12
    • 84983121978 scopus 로고    scopus 로고
    • Development of a discrete-time aerodynamic model for CFD-based aeroelastic analysis
    • AIAA Paper-99-0765, Reno, January
    • T.J. Cowan and A.S. Arena. Development of A Discrete-Time Aerodynamic Model for CFD-Based Aeroelastic Analysis. AIAA Paper-99-0765, 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, January 1999.
    • (1999) 37th AIAA Aerospace Sciences Meeting and Exhibit
    • Cowan, T.J.1    Arena, A.S.2
  • 13
    • 0035078420 scopus 로고    scopus 로고
    • Accelerating computational fluid dynamics based aeroelastic predictions using system identification
    • January-February
    • Cowan, T.J., Arena, A.S. and Gupta, K.K. Accelerating Computational Fluid Dynamics Based Aeroelastic Predictions Using System Identification. Journal of Aircraft, Vol. 38, No. 1, January-February 2001.
    • (2001) Journal of Aircraft , vol.38 , Issue.1
    • Cowan, T.J.1    Arena, A.S.2    Gupta, K.K.3
  • 14
    • 0029696291 scopus 로고    scopus 로고
    • Evolution of flight vehicle system identification
    • Hamel, P.G. and Jategaonkar, R.V. Evolution of Flight Vehicle System Identification. Journal of Aircraft, Vol. 33, No. 1, pp. 9-28, 1996.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 9-28
    • Hamel, P.G.1    Jategaonkar, R.V.2
  • 16
    • 30744459736 scopus 로고    scopus 로고
    • Development of a non-linear indicial model using response functions generated by a neural network
    • Reisenthel, P.H. Development of a Non-linear Indicial Model Using Response Functions Generated by a Neural Network. AIAA Paper-97-0337, 1997.
    • (1997) AIAA Paper-97-0337
    • Reisenthel, P.H.1
  • 18
    • 85088758735 scopus 로고    scopus 로고
    • Flutter predictions by a filtered impulse method
    • Aug.
    • Liu, F., Cai, J., and Tsai, H.M. Flutter Predictions by a Filtered Impulse Method. AIAA Paper-2000-4230, Aug. 2000.
    • (2000) AIAA Paper-2000-4230
    • Liu, F.1    Cai, J.2    Tsai, H.M.3
  • 20
    • 0024880831 scopus 로고
    • Multilayer feedforward networks are universal approximators
    • Hornik, K., Stinchcombe, M. and White, H. Multilayer Feedforward Networks are Universal Approximators. Neural Networks. Vol. 2. pp. 359-366, 1989.
    • (1989) Neural Networks , vol.2 , pp. 359-366
    • Hornik, K.1    Stinchcombe, M.2    White, H.3
  • 21
    • 0024991997 scopus 로고
    • Networks and the best approximation property
    • Poggio, T. and Girosi, F. Networks and the Best Approximation Property. Biological Cybernetics. Vol. 63. pp. 169-176, 1989.
    • (1989) Biological Cybernetics , vol.63 , pp. 169-176
    • Poggio, T.1    Girosi, F.2
  • 23
    • 21144433756 scopus 로고    scopus 로고
    • Comprehensive survey of fitness approximation in evolutionary computation
    • Springer-Verlag
    • Jin, Y. A Comprehensive Survey of Fitness Approximation in Evolutionary Computation. Soft Computing, Springer-Verlag, 2003.
    • (2003) Soft Computing
    • Jin, Y.A.1
  • 24
    • 0003413187 scopus 로고    scopus 로고
    • Prentice Hall Internal Inc., New Jersey
    • nd Edition, Prentice Hall Internal Inc., New Jersey, 1999.
    • (1999) nd Edition
    • Haykin, S.1
  • 27
    • 0004854858 scopus 로고
    • Fully-implicit time-marching aeroelastic solutions
    • Jan
    • Alonso, J.J. and Jameson, A. Fully-Implicit Time-Marching Aeroelastic Solutions. AIAA Paper-94-0056, Jan 1994.
    • (1994) AIAA Paper-94-0056
    • Alonso, J.J.1    Jameson, A.2
  • 28
    • 0035369438 scopus 로고    scopus 로고
    • Unsteady flow calculations with a multi-block moving mesh algorithm
    • Tsai, H.M., Wong, A.S.F., Cai, J., Zhu, Y., and Liu, F. Unsteady Flow Calculations with a Multi-Block Moving Mesh Algorithm. AIAA Journal, Vol. 39, No. 6, pp. 1021-1029, 2001.
    • (2001) AIAA Journal , vol.39 , Issue.6 , pp. 1021-1029
    • Tsai, H.M.1    Wong, A.S.F.2    Cai, J.3    Zhu, Y.4    Liu, F.5
  • 29
    • 0030472979 scopus 로고    scopus 로고
    • Unsteady flow calculations with a multigrid Navier-Stokes method
    • Oct.
    • Liu, F. and Ji, S. Unsteady Flow Calculations with a Multigrid Navier-Stokes Method. AIAA Journal, Vol. 34, No. 10, pp. 2047-2053, Oct. 1996.
    • (1996) AIAA Journal , vol.34 , Issue.10 , pp. 2047-2053
    • Liu, F.1    Ji, S.2
  • 30
    • 0018493237 scopus 로고
    • On the transonic-dip mechanism of flutter of a sweptback wing
    • July
    • Isogai, K. On the Transonic-Dip Mechanism of Flutter of a Sweptback Wing. AIAA Journal, Vol. 17, No. 7, pp. 793-795, July 1979.
    • (1979) AIAA Journal , vol.17 , Issue.7 , pp. 793-795
    • Isogai, K.1
  • 31
    • 0019613591 scopus 로고
    • Transonic dip mechanism of flutter of a sweptback wing: Part II
    • Sept.
    • Isogai, K. Transonic Dip Mechanism of Flutter of a Sweptback Wing: Part II. AIAA Journal, Vol. 19, No. 9, pp. 1240-1242, Sept. 1981.
    • (1981) AIAA Journal , vol.19 , Issue.9 , pp. 1240-1242
    • Isogai, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.