메뉴 건너뛰기




Volumn 1, Issue , 2005, Pages 558-576

Non-linear impulse methods for aero-elastic simulations

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; IMPULSE RESPONSE; IMPULSE TESTING; MATHEMATICAL MODELS; MODAL ANALYSIS;

EID: 28844483013     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-4845     Document Type: Conference Paper
Times cited : (17)

References (35)
  • 2
    • 0017932980 scopus 로고
    • Computation of unsteady transonic flows by the indicial method
    • Ballhaus, W. F. and Goorjlan, P. M., "Computation of Unsteady Transonic Flows by the Indicial Method," AIAA Journal, Vol. 16, No. 2, 1978, pp. 117-124.
    • (1978) AIAA Journal , vol.16 , Issue.2 , pp. 117-124
    • Ballhaus, W.F.1    Goorjlan, P.M.2
  • 4
    • 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, 2001, pp. 1021-1029.
    • (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
  • 5
    • 0035272355 scopus 로고    scopus 로고
    • Calculation of wing flutter by a coupled fluid-structure method
    • 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, 2001, pp. 334-342.
    • (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
  • 6
    • 0346179635 scopus 로고
    • An adaptive cartesian grid method for unsteady compressible flow in irregular regions
    • Pember, R. B., Bell, J. B., and Collela, P., "An Adaptive Cartesian Grid Method for Unsteady Compressible Flow in Irregular Regions," Journal of Computational Physics, Vol. 120, 1995, pp. 278-304.
    • (1995) Journal of Computational Physics , vol.120 , pp. 278-304
    • Pember, R.B.1    Bell, J.B.2    Collela, P.3
  • 7
    • 2942730074 scopus 로고
    • 3D applications of a cartesian grid euler method
    • Melton, J. E., Berger, M. J., Aftosmis, M. J., and Wong, M. D., "3D Applications of A Cartesian Grid Euler Method," AIAA Paper 1995-0853, 1995.
    • (1995) AIAA Paper , vol.1995 , Issue.853
    • Melton, J.E.1    Berger, M.J.2    Aftosmis, M.J.3    Wong, M.D.4
  • 8
    • 0000307275 scopus 로고    scopus 로고
    • A higher order boundary treatment for cartesian-grid methods
    • Forrer, H. and Jeltsch, R., "A Higher Order Boundary Treatment for Cartesian-Grid Methods," Journal of Computational Physics, Vol. 140, 1998, pp. 259-277.
    • (1998) Journal of Computational Physics , vol.140 , pp. 259-277
    • Forrer, H.1    Jeltsch, R.2
  • 9
    • 84894451702 scopus 로고    scopus 로고
    • Simulation of flow around moving 3D body on unstructured cartesian grid
    • June
    • Lahur, P. R. and Nakamura, Y., "Simulation of Flow around Moving 3D Body on Unstructured Cartesian Grid." AIAA Paper 2001-2605, June 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.2605
    • Lahur, P.R.1    Nakamura, Y.2
  • 12
    • 34147197450 scopus 로고
    • An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flows
    • June
    • Sankar, L., Malone, J., and Tassa, Y., "An Implicit Conservative Algorithm for Steady and Unsteady Three-Dimensional Transonic Potential Flows," AIAA Paper 1981-1016, June 1981.
    • (1981) AIAA Paper , vol.1981 , Issue.1016
    • Sankar, L.1    Malone, J.2    Tassa, Y.3
  • 13
    • 0023119573 scopus 로고
    • Euler solutions for transonic flow past a fighter wing
    • Jan.
    • Sankar, L., Malone, J., and Schuster, D., "Euler Solutions for Transonic Flow Past a Fighter Wing," Journal of Aircraft, Vol. 24, No. 1, Jan. 1987, pp. 10-16.
    • (1987) Journal of Aircraft , vol.24 , Issue.1 , pp. 10-16
    • Sankar, L.1    Malone, J.2    Schuster, D.3
  • 14
    • 85087190272 scopus 로고    scopus 로고
    • Calculation of airfoil flutter by an euler method with approximate boundary conditions
    • June
    • Fisher, C. C. and Arena, A. S., "Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary Conditions," AIAA Paper 2003-3830, June 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.3830
    • Fisher, C.C.1    Arena, A.S.2
  • 16
    • 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, 1993, pp. 660-680.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 660-680
    • Silva, W.A.1
  • 17
    • 85081437503 scopus 로고    scopus 로고
    • Flutter predictions by a filtered impulse method
    • Aug.
    • Liu, F., Cal, J., and Tsai, H. M., "Flutter Predictions by a Filtered Impulse Method," AIAA Paper 2000-4230, Aug., 2000.
    • (2000) AIAA Paper , vol.2000 , Issue.4230
    • Liu, F.1    Cal, J.2    Tsai, H.M.3
  • 18
    • 0035078420 scopus 로고    scopus 로고
    • Accelerating computational fluid dynamics based aeroelastic predictions using system identification
    • Jan,-Feb.
    • 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, Jan,-Feb., 2001.
    • (2001) Journal of Aircraft , vol.38 , Issue.1
    • Cowan, T.J.1    Arena, A.S.2    Gupta, K.K.3
  • 19
    • 0030588002 scopus 로고    scopus 로고
    • A strongly-coupled time-marching method for solving the navier-stokes and k-ω turbulence model equations with multigrid
    • Liu, F. and Zheng, X., "A Strongly-Coupled Time-Marching Method for Solving the Navier-Stokes and k-ω Turbulence Model Equations with Multigrid," Journal of Computational Physics, Vol. 128, 1996, pp. 289-300.
    • (1996) Journal of Computational Physics , vol.128 , pp. 289-300
    • Liu, F.1    Zheng, X.2
  • 20
    • 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, Oct. 1996, pp. 2047-2053.
    • (1996) AIAA Journal , vol.34 , Issue.10 , pp. 2047-2053
    • Liu, F.1    Ji, S.2
  • 21
    • 0003655741 scopus 로고
    • Numerical solutions of the euler equations by finite volume methods using runge-kutta time-stepping schemes
    • Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes," AIAA Paper 81-1259, 1981.
    • (1981) AIAA Paper , vol.81 , Issue.1259
    • Jameson, A.1    Schmidt, W.2    Turkel, E.3
  • 22
    • 85067320709 scopus 로고    scopus 로고
    • A CFD and CSD interaction algorithm for large and complex configurations
    • Lai, K. L., Tsai, H. M., and Lum, K. Y., "A CFD and CSD Interaction Algorithm for Large and Complex Configurations," AIAA Paper 2002-2715, 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.2715
    • Lai, K.L.1    Tsai, H.M.2    Lum, K.Y.3
  • 23
    • 20544438500 scopus 로고    scopus 로고
    • Application of three-dlmensional interfaces for data transfer in aeroelastic computations
    • Sadeghl, M., Liu, F., Lai, K. L., and Tsai, H. M., "Application of Three-Dlmensional Interfaces for Data Transfer in Aeroelastic Computations," AIAA Paper 2004-5376, 2004.
    • (2004) AIAA Paper , vol.2004 , Issue.5376
    • Sadeghl, M.1    Liu, F.2    Lai, K.L.3    Tsai, H.M.4
  • 24
    • 0020502578 scopus 로고
    • Some recent applications of XTRAN3S
    • July
    • Seidel, D., Bennet, R., and Ricketts, R., "Some Recent Applications of XTRAN3S," AIAA Paper 1983-1811, July, 1983.
    • (1983) AIAA Paper , vol.1983 , Issue.1811
    • Seidel, D.1    Bennet, R.2    Ricketts, R.3
  • 25
    • 0015160179 scopus 로고
    • Approximate true damping solution of the flutter equation by determinant iteration
    • Hassig, H. J., "Approximate True Damping Solution of the Flutter Equation by Determinant Iteration," Journal of Aircraft, Vol. 8, No. 11, 1971, pp. 885-889.
    • (1971) Journal of Aircraft , vol.8 , Issue.11 , pp. 885-889
    • Hassig, H.J.1
  • 26
    • 0009234093 scopus 로고
    • On the use of indicial function concept in the analysis of unsteady motions of wings and wing-tail combinations
    • Tobak, M., "On the Use of Indicial Function Concept in the Analysis of Unsteady Motions of Wings and Wing-Tail Combinations," NACA Rept. 1188, 1954.
    • (1954) NACA Rept. , vol.1188
    • Tobak, M.1
  • 27
    • 0024880831 scopus 로고
    • Multilayer feedforward networks are universal approxlmators
    • Hornik, K., Stlnchcombe, M., and White, H., "Multilayer Feedforward Networks are Universal Approxlmators," Neural Networks, Vol. 2, 1989, pp. 359-366.
    • (1989) Neural Networks , vol.2 , pp. 359-366
    • Hornik, K.1    Stlnchcombe, M.2    White, H.3
  • 28
    • 0024991997 scopus 로고
    • Networks and the best approximation property
    • Poggio, T. and Girosi, F., "Networks and the Best Approximation Property," Biological Cybernetics, Vol. 63, 1989, pp. 169-176.
    • (1989) Biological Cybernetics , vol.63 , pp. 169-176
    • Poggio, T.1    Girosi, F.2
  • 30
    • 21144433756 scopus 로고    scopus 로고
    • A 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.1
  • 31
    • 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
  • 34
    • 0008737498 scopus 로고
    • Measured and calculated subsonic and transonic flutter characteristics of a 45° sweptback wing planform in air and in freon-12 in the langley transonic dynamics tunnel
    • Yates, E. C., Land, N. S., and Foughner, J. T., "Measured and Calculated Subsonic and Transonic Flutter Characteristics of a 45° Sweptback Wing Planform in Air and in Freon-12 in the Langley Transonic Dynamics Tunnel," AGARD TN D-1616, 1963.
    • (1963) AGARD TN , vol.D-1616
    • Yates, E.C.1    Land, N.S.2    Foughner, J.T.3
  • 35
    • 0004826888 scopus 로고
    • AGARD standard aeroelastic configurations for dynamic response I - Wing 445.6
    • Aug.
    • "AGARD Standard Aeroelastic Configurations for Dynamic Response I - Wing 445.6," NASA TM 100492, Aug., 1987.
    • (1987) NASA TM 100492


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.