메뉴 건너뛰기




Volumn 365, Issue 1859, 2007, Pages 2469-2499

Computational aeroelastic modelling of airframes and turbomachinery: Progress and challenges

Author keywords

Airframes; Computational aeroelasticity; Computational fluid dynamics; Turbomachinery

Indexed keywords


EID: 34748869055     PISSN: 1364503X     EISSN: None     Source Type: Journal    
DOI: 10.1098/rsta.2007.2018     Document Type: Article
Times cited : (35)

References (127)
  • 1
    • 85007685430 scopus 로고
    • A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
    • Albano, E. & Rodden, W. P. 1969 A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. AIAA J. 7, 279-285.
    • (1969) AIAA J , vol.7 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 4
    • 29544439860 scopus 로고    scopus 로고
    • Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing
    • doi:10.1016/j.jfluidstructs.2005.08.010
    • Attar, P. J. & Gordnier, R. E. 2006 Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing. J. Fluid Struct. 22, 45-58. (doi:10.1016/j.jfluidstructs.2005.08.010)
    • (2006) J. Fluid Struct , vol.22 , pp. 45-58
    • Attar, P.J.1    Gordnier, R.E.2
  • 5
    • 0036651053 scopus 로고    scopus 로고
    • Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface
    • Bae, J.-S., Yang, S.-M. & Lee, I. 2002 Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface. J. Aircraft 39, 697-708.
    • (2002) J. Aircraft , vol.39 , pp. 697-708
    • Bae, J.-S.1    Yang, S.-M.2    Lee, I.3
  • 6
    • 85020800433 scopus 로고    scopus 로고
    • Bartels, R. E, Rumsey, C. L. & Biedron, R. T. 2006 CFL3D Version 6.4, General usage and aeroelastic analysis. NASA/TM-2006-214301
    • Bartels, R. E., Rumsey, C. L. & Biedron, R. T. 2006 CFL3D Version 6.4 - General usage and aeroelastic analysis. NASA/TM-2006-214301.
  • 7
    • 34748862866 scopus 로고    scopus 로고
    • Advanced small perturbation potential flow theory for unsteady aerodynamic and aeroelastic analyses
    • Batina, J. T. 2005 Advanced small perturbation potential flow theory for unsteady aerodynamic and aeroelastic analyses. NASA TM 2005-213908.
    • (2005) NASA TM , pp. 2005-213908
    • Batina, J.T.1
  • 8
    • 0024301791 scopus 로고
    • Unsteady transonic flow calculations for realistic aircraft configurations
    • Batina, J. T., Seidel, D. A., Bland, R. R. & Bennet, R. M. 1989 Unsteady transonic flow calculations for realistic aircraft configurations. J. Aircraft 26, 21-28.
    • (1989) J. Aircraft , vol.26 , pp. 21-28
    • Batina, J.T.1    Seidel, D.A.2    Bland, R.R.3    Bennet, R.M.4
  • 12
    • 0034273920 scopus 로고    scopus 로고
    • Limit cycle oscillation characteristics of fighter aircraft
    • Bunton, R. W. & Denegri, C. M. 2000 Limit cycle oscillation characteristics of fighter aircraft. J. Aircraft 37, 916-918.
    • (2000) J. Aircraft , vol.37 , pp. 916-918
    • Bunton, R.W.1    Denegri, C.M.2
  • 14
    • 34748901093 scopus 로고
    • The role of acoustic resonances in unsteady turbomachinery aerodynamics
    • Cargill, A. M. 1987 The role of acoustic resonances in unsteady turbomachinery aerodynamics. In Proc. 4th ISUAAT Symposium, Aachen.
    • (1987) Proc. 4th ISUAAT Symposium, Aachen
    • Cargill, A.M.1
  • 16
    • 0346973054 scopus 로고    scopus 로고
    • Coupled simulation of flow-structure interactions in turbomachinery
    • doi:10.1016/S1270-9638(03)00016-6
    • Carstens, V., Kemme, R. & Schmitt, S. 2003 Coupled simulation of flow-structure interactions in turbomachinery. Aerosp. Sci. Technol. 7, 298-306. (doi:10.1016/S1270-9638(03)00016-6)
    • (2003) Aerosp. Sci. Technol , vol.7 , pp. 298-306
    • Carstens, V.1    Kemme, R.2    Schmitt, S.3
  • 17
    • 0030790699 scopus 로고    scopus 로고
    • Conservative load projection and tracking for fluid-structure problems
    • Cebral, J. R. & Lohner, R. 1997 Conservative load projection and tracking for fluid-structure problems. AIAA J. 35, 687-692.
    • (1997) AIAA J , vol.35 , pp. 687-692
    • Cebral, J.R.1    Lohner, R.2
  • 18
    • 0141796591 scopus 로고    scopus 로고
    • Nonlinear response of aeroservoelastic systems using discrete state-space approach
    • Chen, P. C. & Sulaeman, E. 2003 Nonlinear response of aeroservoelastic systems using discrete state-space approach. AIAA J. 41, 1658-1666.
    • (2003) AIAA J , vol.41 , pp. 1658-1666
    • Chen, P.C.1    Sulaeman, E.2
  • 20
    • 0033875096 scopus 로고    scopus 로고
    • Transonic-aerodynamic- influence-coefficient approach for aeroelastic and MDO applications
    • Chen, P. C., Sarhaddi, D. & Liu, D. D. 2000 Transonic-aerodynamic- influence-coefficient approach for aeroelastic and MDO applications. J. Aircraft 37, 85-94.
    • (2000) J. Aircraft , vol.37 , pp. 85-94
    • Chen, P.C.1    Sarhaddi, D.2    Liu, D.D.3
  • 22
    • 85020835425 scopus 로고    scopus 로고
    • Cizmas, P. G. A. & Hall, K. C. 1995 A viscous-inviscid model of unsteady small-disturbance flows in cascades. AIAA Paper 95-2655.
    • Cizmas, P. G. A. & Hall, K. C. 1995 A viscous-inviscid model of unsteady small-disturbance flows in cascades. AIAA Paper 95-2655.
  • 23
    • 0000283402 scopus 로고
    • The expanding domain of aeroelasticity
    • Collar, A. R. 1946 The expanding domain of aeroelasticity. J. R. Aeronaut. Soc. 50, 613-636.
    • (1946) J. R. Aeronaut. Soc , vol.50 , pp. 613-636
    • Collar, A.R.1
  • 24
    • 0002535971 scopus 로고
    • The first fifty years of aeroelasticity
    • Collar, A. R. 1978 The first fifty years of aeroelasticity. Aerospace 5, 12-20.
    • (1978) Aerospace , vol.5 , pp. 12-20
    • Collar, A.R.1
  • 25
    • 0036998208 scopus 로고    scopus 로고
    • Contreras, J., Corral, R., Fernandez-Castaneda, J., Pastor, G. & Vasco, C. 2002 Semiunstructured grid methods for turbomachinery applications. ASME Turbo Expo. GT-2002-30572.
    • Contreras, J., Corral, R., Fernandez-Castaneda, J., Pastor, G. & Vasco, C. 2002 Semiunstructured grid methods for turbomachinery applications. ASME Turbo Expo. GT-2002-30572.
  • 26
    • 0035959238 scopus 로고    scopus 로고
    • Airbus elevator flutter: Annoying or dangerous?
    • Croft, J. 2001 Airbus elevator flutter: annoying or dangerous? Aviat. Week Space Technol. 155, 41.
    • (2001) Aviat. Week Space Technol , vol.155 , pp. 41
    • Croft, J.1
  • 27
    • 0036991461 scopus 로고    scopus 로고
    • Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery
    • Doi, H. & Alonso, J. J. 2002 Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery. ASME Turbo Expo. GT-2002-30313.
    • (2002) ASME Turbo Expo. GT-2002-30313
    • Doi, H.1    Alonso, J.J.2
  • 29
    • 18144401335 scopus 로고    scopus 로고
    • In-flight wing deformation characteristics during limit-cycle oscillations
    • Denegri, C. M., Dubben, J. A. & Maxwell, D. L. 2005 In-flight wing deformation characteristics during limit-cycle oscillations. J. Aircraft 42, 500-508.
    • (2005) J. Aircraft , vol.42 , pp. 500-508
    • Denegri, C.M.1    Dubben, J.A.2    Maxwell, D.L.3
  • 32
    • 0020846613 scopus 로고
    • Time-marching transonic flutter solutions including angle-of-attack effects
    • Edwards, J. W., Bennett, R. M., Whitlow, W. & Seidel, D. A. 1983 Time-marching transonic flutter solutions including angle-of-attack effects. J. Aircraft 20, 899-906.
    • (1983) J. Aircraft , vol.20 , pp. 899-906
    • Edwards, J.W.1    Bennett, R.M.2    Whitlow, W.3    Seidel, D.A.4
  • 33
    • 0001759089 scopus 로고    scopus 로고
    • Reduced-order models of unsteady transonic viscous flows in turbomachinery
    • doi:10.1006/jfls.2000.0320
    • Epureanu, B. I., Dowell, E. H. & Hall, K. C. 2000 Reduced-order models of unsteady transonic viscous flows in turbomachinery. J. Fluid Struct. 14, 1215-1234. (doi:10.1006/jfls.2000.0320)
    • (2000) J. Fluid Struct , vol.14 , pp. 1215-1234
    • Epureanu, B.I.1    Dowell, E.H.2    Hall, K.C.3
  • 34
    • 0017554663 scopus 로고
    • Numerical solution of periodic transonic flow through a fan stage
    • Erdos, J. I., Alzner, E. & McNally, W. 1977 Numerical solution of periodic transonic flow through a fan stage. AIAA J. 15, 1559-1568.
    • (1977) AIAA J , vol.15 , pp. 1559-1568
    • Erdos, J.I.1    Alzner, E.2    McNally, W.3
  • 35
    • 0032053181 scopus 로고    scopus 로고
    • Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and energy conservation, optimal discretization and application to aeroelasticity
    • doi:10.1016/S0045-7825(97)00216-8
    • Farhat, C., Lesoinne, M. & LeTallec, P. 1998 Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: momentum and energy conservation, optimal discretization and application to aeroelasticity. Comput. Methods Appl. Mech. Eng. 157, 95-114. (doi:10.1016/S0045-7825(97)00216-8)
    • (1998) Comput. Methods Appl. Mech. Eng , vol.157 , pp. 95-114
    • Farhat, C.1    Lesoinne, M.2    LeTallec, P.3
  • 36
    • 0036390834 scopus 로고    scopus 로고
    • Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
    • doi:10.1016/S0045-7930(01)00104-9
    • Farhat, C., Geuzaine, P. & Brown, G. 2003 Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter. Comput. Fluid 32, 3-29. (doi:10.1016/S0045-7930(01)00104-9)
    • (2003) Comput. Fluid , vol.32 , pp. 3-29
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3
  • 37
    • 32044458550 scopus 로고    scopus 로고
    • Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
    • doi:10.1016/j.cma.2004.11.031
    • Farhat, C., van der Zee, K. G. & Geuzaine, P. 2006 Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity. Comput. Methods Appl. Mech. Eng. 195, 1973-2001. (doi:10.1016/j.cma.2004.11.031)
    • (2006) Comput. Methods Appl. Mech. Eng , vol.195 , pp. 1973-2001
    • Farhat, C.1    van der Zee, K.G.2    Geuzaine, P.3
  • 38
    • 0032757223 scopus 로고    scopus 로고
    • The renaissance of aeroelasticity and its future
    • Friedmann, P. P. 1999 The renaissance of aeroelasticity and its future. J. Aircraft 36, 105-121.
    • (1999) J. Aircraft , vol.36 , pp. 105-121
    • Friedmann, P.P.1
  • 39
    • 0007550915 scopus 로고
    • An unstructured-grid software system for solving complex aerodynamic problems
    • Frink, N. T., Pirzadeh, S. & Parikh, P. 1995 An unstructured-grid software system for solving complex aerodynamic problems. NASA CP-3291. 289-308.
    • (1995) NASA CP-3291 , pp. 289-308
    • Frink, N.T.1    Pirzadeh, S.2    Parikh, P.3
  • 40
    • 24144457003 scopus 로고    scopus 로고
    • Numerical investigation of nonlinear aeroelastic effects on flexible high-aspect-ratio wings
    • Garcia, J. A. 2005 Numerical investigation of nonlinear aeroelastic effects on flexible high-aspect-ratio wings. J. Aircraft 42, 1025-1036.
    • (2005) J. Aircraft , vol.42 , pp. 1025-1036
    • Garcia, J.A.1
  • 41
    • 0023572407 scopus 로고
    • Analysis of unsteady aerodynamics for elastic bodies in supersonic flow
    • Garcia-Fogeda, P. & Liu, D. D. 1987 Analysis of unsteady aerodynamics for elastic bodies in supersonic flow. J. Aircraft 24, 833-840.
    • (1987) J. Aircraft , vol.24 , pp. 833-840
    • Garcia-Fogeda, P.1    Liu, D.D.2
  • 42
    • 0016996419 scopus 로고
    • Aeroelasticity - frontiers and beyond. 13th Von Karman Lecture
    • Garrick, I. E. 1976 Aeroelasticity - frontiers and beyond. 13th Von Karman Lecture. AIAA J. Aircraft 13, 641-657.
    • (1976) AIAA J. Aircraft , vol.13 , pp. 641-657
    • Garrick, I.E.1
  • 43
    • 0019633695 scopus 로고
    • Historical development of aircraft flutter
    • Garrick, I. E. & Reed, W. H. 1981 Historical development of aircraft flutter. AIAA J. Aircraft 18, 897-912.
    • (1981) AIAA J. Aircraft , vol.18 , pp. 897-912
    • Garrick, I.E.1    Reed, W.H.2
  • 44
    • 0141570811 scopus 로고    scopus 로고
    • Design and analysis of ALE schemes with provable second-order time-accuracy for inviscid and viscous flow simulations
    • doi:10.1016/S0021-9991(03)00311-5
    • Geuzaine, P., Grandmont, C. & Farhat, C. 2003 Design and analysis of ALE schemes with provable second-order time-accuracy for inviscid and viscous flow simulations. J. Comput. Phys. 191, 206-227. (doi:10.1016/S0021-9991(03)00311-5)
    • (2003) J. Comput. Phys , vol.191 , pp. 206-227
    • Geuzaine, P.1    Grandmont, C.2    Farhat, C.3
  • 45
    • 0024050478 scopus 로고
    • Calculation of unsteady wake/rotor interaction
    • Giles, M. B. 1988 Calculation of unsteady wake/rotor interaction. AIAA J. Propul. Power 4, 356-362.
    • (1988) AIAA J. Propul. Power , vol.4 , pp. 356-362
    • Giles, M.B.1
  • 46
    • 85020799351 scopus 로고    scopus 로고
    • Giles, M. B. 1992 SLIQ: an approach for multi-stage calculations incorporating unsteadiness, ASME Paper 92-GT-282.
    • Giles, M. B. 1992 SLIQ: an approach for multi-stage calculations incorporating unsteadiness, ASME Paper 92-GT-282.
  • 48
    • 0346093756 scopus 로고    scopus 로고
    • Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft wing
    • doi:10.1016/S1270-9638(02)00007-X
    • Girodroux-Lavigne, P., Grisval, J. P., Guillemot, S., Henshaw, M., Karlsson, A., Selmin, V., Smith, J., Teupootahiti, E. & Winzell, B. 2003 Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft wing. Aerospace Sci. Technol. 7, 121-133. (doi:10.1016/S1270-9638(02)00007-X)
    • (2003) Aerospace Sci. Technol , vol.7 , pp. 121-133
    • Girodroux-Lavigne, P.1    Grisval, J.P.2    Guillemot, S.3    Henshaw, M.4    Karlsson, A.5    Selmin, V.6    Smith, J.7    Teupootahiti, E.8    Winzell, B.9
  • 50
    • 0025401898 scopus 로고
    • Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
    • Guruswamy, G. P. 1990 Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations. AIAA J. 28, 461-469.
    • (1990) AIAA J , vol.28 , pp. 461-469
    • Guruswamy, G.P.1
  • 51
    • 0027556095 scopus 로고
    • Linearised Euler predictions of unsteady aerodynamic loads in cascades
    • Hall, K. C. & Clark, W. S. 1993 Linearised Euler predictions of unsteady aerodynamic loads in cascades. AIAA J. 31, 540-550.
    • (1993) AIAA J , vol.31 , pp. 540-550
    • Hall, K.C.1    Clark, W.S.2
  • 52
    • 0024673636 scopus 로고
    • Calculation of unsteady flows in turbomachinery using the linearised Euler equations
    • Hall, K. C. & Crawley, E. 1989 Calculation of unsteady flows in turbomachinery using the linearised Euler equations. AIAA J. 27, 777-787.
    • (1989) AIAA J , vol.27 , pp. 777-787
    • Hall, K.C.1    Crawley, E.2
  • 53
    • 15944370032 scopus 로고    scopus 로고
    • Multistage coupling for unsteady flows in turbomachinery
    • Hall, K. & Kivanc, E. 2005 Multistage coupling for unsteady flows in turbomachinery. AIAA J. 43, 624-632.
    • (2005) AIAA J , vol.43 , pp. 624-632
    • Hall, K.1    Kivanc, E.2
  • 54
    • 0027683647 scopus 로고
    • Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic Euler equations
    • Hall, K. C. & Lorence, C. B. 1993 Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic Euler equations. J. Turbomach. 115, 800-809.
    • (1993) J. Turbomach , vol.115 , pp. 800-809
    • Hall, K.C.1    Lorence, C.B.2
  • 55
    • 0028467844 scopus 로고    scopus 로고
    • A linearized Euler analysis of unsteady transonic flows in turbo-machinery
    • Hall, K. C., Clark, W. S. & Lorence, C. B. 1999 A linearized Euler analysis of unsteady transonic flows in turbo-machinery. J. Turbomach. 116, 477-488.
    • (1999) J. Turbomach , vol.116 , pp. 477-488
    • Hall, K.C.1    Clark, W.S.2    Lorence, C.B.3
  • 56
    • 0036572063 scopus 로고    scopus 로고
    • Computation of unsteady nonlinear flows in cascades using a harmonic balance technique
    • Hall, K. C., Thomas, J. P. & Clark, W. S. 2002 Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. AIAA J. 40, 879-886.
    • (2002) AIAA J , vol.40 , pp. 879-886
    • Hall, K.C.1    Thomas, J.P.2    Clark, W.S.3
  • 58
    • 0015291061 scopus 로고
    • Interpolation using surface splines
    • Harder, R. L. & Desmarais, R. N. 1972 Interpolation using surface splines. J. Aircraft 9, 189-191.
    • (1972) J. Aircraft , vol.9 , pp. 189-191
    • Harder, R.L.1    Desmarais, R.N.2
  • 59
    • 0027187076 scopus 로고
    • Inviscid-viscous coupled solution for unsteady flows through vibrating blades: Part 1
    • He, L. & Denton, J. D. 1993 Inviscid-viscous coupled solution for unsteady flows through vibrating blades: part 1. ASME J. Turbomach. 115, 94-100.
    • (1993) ASME J. Turbomach , vol.115 , pp. 94-100
    • He, L.1    Denton, J.D.2
  • 60
    • 0037000724 scopus 로고    scopus 로고
    • He, L., Chen, T., Wells, R. G., Li, Y. S. & Ning, W. 2002 Analysis of rotor-rotor and stator-stator interferences in multi-stage turbomachines. ASME Turbo Expo. GT-2002-30355.
    • He, L., Chen, T., Wells, R. G., Li, Y. S. & Ning, W. 2002 Analysis of rotor-rotor and stator-stator interferences in multi-stage turbomachines. ASME Turbo Expo. GT-2002-30355.
  • 61
    • 84878625967 scopus 로고    scopus 로고
    • Progress of the viscous-coupled 3D Euler method EUVISC and its aeroelastic application
    • Amsterdam, The Netherlands
    • Henke, H. H. 2003 Progress of the viscous-coupled 3D Euler method EUVISC and its aeroelastic application. In Int. Forum on Aeroelasticity and Structural Dynamics. Amsterdam, The Netherlands.
    • (2003) Int. Forum on Aeroelasticity and Structural Dynamics
    • Henke, H.H.1
  • 62
    • 85020800309 scopus 로고    scopus 로고
    • Holmes, D. G., Mitchell, B. E. & Lorence, C. B. 1997 Three dimensional linearized Navier-Stokes calculations for flutter and forced response. In the 8th International Symposium on Unsteady Aerodynamics and Aeroelasticity of Turbomachines (ISUAAT). Stockholm, pp. 211-224.
    • Holmes, D. G., Mitchell, B. E. & Lorence, C. B. 1997 Three dimensional linearized Navier-Stokes calculations for flutter and forced response. In the 8th International Symposium on Unsteady Aerodynamics and Aeroelasticity of Turbomachines (ISUAAT). Stockholm, pp. 211-224.
  • 64
    • 10644233843 scopus 로고    scopus 로고
    • Common-refinement-based data transfer between non-matching meshes in multiphysics simulations
    • doi: 10.1002/nme.1147
    • Jiao, X. & Heath, M. T. 2004 Common-refinement-based data transfer between non-matching meshes in multiphysics simulations. Int. J. Numer. Methods Eng. 61, 2402-2427. (doi: 10.1002/nme.1147)
    • (2004) Int. J. Numer. Methods Eng , vol.61 , pp. 2402-2427
    • Jiao, X.1    Heath, M.T.2
  • 66
    • 15344349684 scopus 로고    scopus 로고
    • Fluid-structure interaction for aeroelastic applications
    • doi:10.1016/j.paerosci.2005.01.001
    • Kamakoti, R. & Shyy, W. 2004 Fluid-structure interaction for aeroelastic applications. Prog. Aerosp. Sci. 40, 535-558. (doi:10.1016/j.paerosci.2005.01.001)
    • (2004) Prog. Aerosp. Sci , vol.40 , pp. 535-558
    • Kamakoti, R.1    Shyy, W.2
  • 67
    • 29544443507 scopus 로고    scopus 로고
    • Aeroelastic model reduction for affordable computational fluid dynamics-based flutter analysis
    • Kim, T., Hong, M., Bhatia, K. & SenGupta, G. 2005 Aeroelastic model reduction for affordable computational fluid dynamics-based flutter analysis. AIAA J. 43, 2487-2495.
    • (2005) AIAA J , vol.43 , pp. 2487-2495
    • Kim, T.1    Hong, M.2    Bhatia, K.3    SenGupta, G.4
  • 69
    • 0029277237 scopus 로고
    • Wing flutter boundary prediction using unsteady Euler method
    • Lee-Rausch, E. M. & Batina, J. T. 1995 Wing flutter boundary prediction using unsteady Euler method. J. Aircraft 32, 416-422.
    • (1995) J. Aircraft , vol.32 , pp. 416-422
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 70
    • 0030289123 scopus 로고    scopus 로고
    • Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations
    • Lee-Rausch, E. M. & Batina, J. T. 1996 Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations. J. Aircraft 33, 1139-1147.
    • (1996) J. Aircraft , vol.33 , pp. 1139-1147
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 71
    • 0026219721 scopus 로고
    • Further studies of harmonic gradient method for supersonic aeroelastic applications
    • Liu, D. D., James, D. K., Chen, P. C. & Pototzky, A. S. 1991 Further studies of harmonic gradient method for supersonic aeroelastic applications. J. Aircraft 28, 598-605.
    • (1991) J. Aircraft , vol.28 , pp. 598-605
    • Liu, D.D.1    James, D.K.2    Chen, P.C.3    Pototzky, A.S.4
  • 72
    • 0347930308 scopus 로고    scopus 로고
    • The future of airplane aeroelasticity
    • Livne, E. 2003 The future of airplane aeroelasticity. J. Aircraft 40, 1066-1092.
    • (2003) J. Aircraft , vol.40 , pp. 1066-1092
    • Livne, E.1
  • 73
    • 0029256189 scopus 로고
    • Matching fluid and structure meshes for aeroelastic computations: A parallel approach
    • doi:10.1016/0045-7949(94)00359-B
    • Maman, N. & Farhat, C. 1995 Matching fluid and structure meshes for aeroelastic computations: a parallel approach. Comput. Struct. 54, 779-785. (doi:10.1016/0045-7949(94)00359-B)
    • (1995) Comput. Struct , vol.54 , pp. 779-785
    • Maman, N.1    Farhat, C.2
  • 74
    • 0348222733 scopus 로고
    • Adaptive harmonic balance method for nonlinear time-periodic flows
    • doi:10.1016/j.jcp.2003.08.013
    • Maple, R., King, P. L., Orkws, P. D. & Wolf, J. M. 1994 Adaptive harmonic balance method for nonlinear time-periodic flows. J. Comput. Phys. 193, 620-641. (doi:10.1016/j.jcp.2003.08.013)
    • (1994) J. Comput. Phys , vol.193 , pp. 620-641
    • Maple, R.1    King, P.L.2    Orkws, P.D.3    Wolf, J.M.4
  • 75
    • 0029673651 scopus 로고    scopus 로고
    • A review of aeroelasticity methods with emphasis on turbomachinery applications
    • doi:10.1006/jfls.1996.0015
    • Marshall, J. G. & Imregun, M. 1996 A review of aeroelasticity methods with emphasis on turbomachinery applications. J. Fluid Struct. 10, 237-267. (doi:10.1006/jfls.1996.0015)
    • (1996) J. Fluid Struct , vol.10 , pp. 237-267
    • Marshall, J.G.1    Imregun, M.2
  • 80
    • 0016496593 scopus 로고
    • Advances in fan and compressor blade flutter analysis and prediction
    • Mikolajczak, A. A., Arnoldi, R. A., Snyder, L. E. & Stargardter, H. 1975 Advances in fan and compressor blade flutter analysis and prediction. J. Aircraft 12, 325-332.
    • (1975) J. Aircraft , vol.12 , pp. 325-332
    • Mikolajczak, A.A.1    Arnoldi, R.A.2    Snyder, L.E.3    Stargardter, H.4
  • 86
    • 0032124663 scopus 로고    scopus 로고
    • Computation of unsteady flows around oscillating blades using linear and nonlinear harmonic Euler methods
    • Ning, W. & He, L. 1998 Computation of unsteady flows around oscillating blades using linear and nonlinear harmonic Euler methods. J. Turbomach. 120, 508-519.
    • (1998) J. Turbomach , vol.120 , pp. 508-519
    • Ning, W.1    He, L.2
  • 87
    • 85020838809 scopus 로고    scopus 로고
    • Development of a solution for the transonic flutter analysis of finite wings
    • Amsterdam, The Netherlands
    • Nitzsche, F. & Voss, R. 2003 Development of a solution for the transonic flutter analysis of finite wings. In Int. Forum on Aeroelasticity and Structural Dynamics. Amsterdam, The Netherlands.
    • (2003) Int. Forum on Aeroelasticity and Structural Dynamics
    • Nitzsche, F.1    Voss, R.2
  • 89
    • 0022914936 scopus 로고
    • Implicit conservative zonal boundary scheme for Euler equation calculations
    • doi:10.1016/0045-7930(86)90027-7
    • Rai, M. M. 1986 Implicit conservative zonal boundary scheme for Euler equation calculations. Comput. Fluid 14, 295-319. (doi:10.1016/0045-7930(86)90027-7)
    • (1986) Comput. Fluid , vol.14 , pp. 295-319
    • Rai, M.M.1
  • 90
    • 0023407621 scopus 로고
    • Navier-Stokes simulations of rotor/stator interaction using patched and overlaid grids
    • Rai, M. M. 1987 Navier-Stokes simulations of rotor/stator interaction using patched and overlaid grids. AIAA J. Propul. Power 3, 387-396.
    • (1987) AIAA J. Propul. Power , vol.3 , pp. 387-396
    • Rai, M.M.1
  • 91
    • 0027658687 scopus 로고
    • Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method
    • Rausch, R. D., Yang, H. T. Y. & Batina, J. T. 1993 Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method. J. Aircraft 31, 1626-1633.
    • (1993) J. Aircraft , vol.31 , pp. 1626-1633
    • Rausch, R.D.1    Yang, H.T.Y.2    Batina, J.T.3
  • 92
    • 0026261105 scopus 로고
    • Aeroelastic analysis of wings using the Euler equations with a deforming mesh
    • Robinson, B. A., Batina, J. T. & Yang, H. T. Y. 1991 Aeroelastic analysis of wings using the Euler equations with a deforming mesh. J. Aircraft 28, 781-788.
    • (1991) J. Aircraft , vol.28 , pp. 781-788
    • Robinson, B.A.1    Batina, J.T.2    Yang, H.T.Y.3
  • 93
    • 33750856097 scopus 로고    scopus 로고
    • A multi blade-row linearised analysis method for flutter and forced response predictions in turbomachinery
    • GT2006-90789
    • Saiz, G. Imregun, M. & Sayma, A. I. 2006 A multi blade-row linearised analysis method for flutter and forced response predictions in turbomachinery. ASME Turbo Expo. GT2006-90789.
    • (2006) ASME Turbo Expo
    • Saiz, G.1    Imregun, M.2    Sayma, A.I.3
  • 96
    • 0003206778 scopus 로고    scopus 로고
    • Multi-stage whole-annulus forced response predictions using an integrated non-linear analysis technique - part I: Numerical model
    • doi:10.1006/jfls.1999.0253
    • Sayma, A. I., Vahdati, M. & Imregun, M. 2000a Multi-stage whole-annulus forced response predictions using an integrated non-linear analysis technique - part I: numerical model. J. Fluid Struct. 14, 87-101. (doi:10.1006/jfls.1999.0253)
    • (2000) J. Fluid Struct , vol.14 , pp. 87-101
    • Sayma, A.I.1    Vahdati, M.2    Imregun, M.3
  • 97
    • 0034469949 scopus 로고    scopus 로고
    • Multi-bladerow fan forced response predictions using an integrated 3D time-domain aeroelasticity model
    • Sayma, A. I., Vahdati, M. & Imregun, M. 2000b Multi-bladerow fan forced response predictions using an integrated 3D time-domain aeroelasticity model. J. Mech. Eng. Sci. Part C 214, 1467-1483.
    • (2000) J. Mech. Eng. Sci. Part C , vol.214 , pp. 1467-1483
    • Sayma, A.I.1    Vahdati, M.2    Imregun, M.3
  • 98
    • 0034352099 scopus 로고    scopus 로고
    • Sbardella, L. & Imregun, M. 2000 An efficient discretization of viscous fluxes on unstructured mixed-element grids. Commun. Numer. Methods Eng. 16, 839-849. (doi:10.1002/1099-0887 (200012)16:12<839::AID- CNM382>3.0.CO;2-3)
    • Sbardella, L. & Imregun, M. 2000 An efficient discretization of viscous fluxes on unstructured mixed-element grids. Commun. Numer. Methods Eng. 16, 839-849. (doi:10.1002/1099-0887 (200012)16:12<839::AID- CNM382>3.0.CO;2-3)
  • 99
    • 0034652815 scopus 로고    scopus 로고
    • Sbardella, L., Sayma, A. I. & Imregun, M. 1999 Semi-unstructured meshes for axial turbomachinery blades. Int. J. Numer. Methods Fluid 32, 569-584. (doi:10.1002/(SICI)1097-0363 (20000315)32:5<569::AID- FLD975>3.0.CO;2-V)
    • Sbardella, L., Sayma, A. I. & Imregun, M. 1999 Semi-unstructured meshes for axial turbomachinery blades. Int. J. Numer. Methods Fluid 32, 569-584. (doi:10.1002/(SICI)1097-0363 (20000315)32:5<569::AID- FLD975>3.0.CO;2-V)
  • 100
    • 85002537808 scopus 로고
    • Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
    • Schuster, D. M., Vadyak, J. & Atta, E. 1990 Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm. J. Aircraft 27, 820-825.
    • (1990) J. Aircraft , vol.27 , pp. 820-825
    • Schuster, D.M.1    Vadyak, J.2    Atta, E.3
  • 101
    • 0242304914 scopus 로고    scopus 로고
    • Computational aeroelasticity: Success, progress, challenge
    • Schuster, D. M., Liu, D. D. & Huttsell, L. J. 2003 Computational aeroelasticity: success, progress, challenge. J. Aircraft 40, 843-856.
    • (2003) J. Aircraft , vol.40 , pp. 843-856
    • Schuster, D.M.1    Liu, D.D.2    Huttsell, L.J.3
  • 103
    • 2342596443 scopus 로고    scopus 로고
    • Alleviation of vertical tail buffeting of F/A-18 Aircraft
    • Sheta, E. F. 2004 Alleviation of vertical tail buffeting of F/A-18 Aircraft. J. Aircraft 41, 322-330.
    • (2004) J. Aircraft , vol.41 , pp. 322-330
    • Sheta, E.F.1
  • 104
    • 0032124706 scopus 로고    scopus 로고
    • A coupled mode analysis of unsteady multistage flows in turbomachinery
    • Silkowski, P. D. & Hall, K. C. 1998 A coupled mode analysis of unsteady multistage flows in turbomachinery. J. Turbomach. 120, 410-421.
    • (1998) J. Turbomach , vol.120 , pp. 410-421
    • Silkowski, P.D.1    Hall, K.C.2
  • 105
    • 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
    • Silva, W. & Bartels, R. 2004 Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code. J. Fluid Struct. 19, 729-745. (doi:10.1016/j.jfluidstructs.2004.03.004)
    • (2004) J. Fluid Struct , vol.19 , pp. 729-745
    • Silva, W.1    Bartels, R.2
  • 106
    • 0003161776 scopus 로고
    • Stall flutter in cascades
    • Sisto, F. 1953 Stall flutter in cascades. J. Aeronaut. Sci. 20, 598-604.
    • (1953) J. Aeronaut. Sci , vol.20 , pp. 598-604
    • Sisto, F.1
  • 109
    • 0026820445 scopus 로고
    • A new strategy for finite element computations involving moving boundaries and interfaces - the deforming spatial domain/space-time procedure: I. The concept and the preliminary numerical tests
    • doi:10.1016/0045-7825(92)90059-S
    • Tezduyar, T., Behr, M. & Liou, J. 1992 A new strategy for finite element computations involving moving boundaries and interfaces - the deforming spatial domain/space-time procedure: I. The concept and the preliminary numerical tests. Comput. Methods Appl. Mech. Eng. 94, 339-351. (doi:10.1016/0045-7825(92)90059-S)
    • (1992) Comput. Methods Appl. Mech. Eng , vol.94 , pp. 339-351
    • Tezduyar, T.1    Behr, M.2    Liou, J.3
  • 110
    • 32044445726 scopus 로고    scopus 로고
    • Space-time finite element techniques for computation of fluid-structure interaction
    • doi: 10.1016/j.cma.2004.09.014
    • Tezduyar, T. E., Sathe, S., Keedy, R. & Stein, K. 2006 Space-time finite element techniques for computation of fluid-structure interaction. Comput. Methods Appl. Mech. Eng. 195, 2002-2027. (doi: 10.1016/j.cma.2004.09.014)
    • (2006) Comput. Methods Appl. Mech. Eng , vol.195 , pp. 2002-2027
    • Tezduyar, T.E.1    Sathe, S.2    Keedy, R.3    Stein, K.4
  • 111
    • 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. 2002 Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations. AIAA J. 40, 638-646.
    • (2002) AIAA J , vol.40 , pp. 638-646
    • Thomas, J.P.1    Dowell, E.H.2    Hall, K.C.3
  • 115
    • 0030681691 scopus 로고    scopus 로고
    • An application of the ICED-ALE methodology for integrated non-linear aeroelasticity analysis
    • doi:10.1108/02644409710170979
    • Vahdati, M. & Imregun, M. 1997 An application of the ICED-ALE methodology for integrated non-linear aeroelasticity analysis. Eng. Comput. 14, 281-305. (doi:10.1108/02644409710170979)
    • (1997) Eng. Comput , vol.14 , pp. 281-305
    • Vahdati, M.1    Imregun, M.2
  • 116
    • 0001452041 scopus 로고    scopus 로고
    • Multi-stage whole-annulus forced response predictions using an integrated non-linear analysis technique - part II: Study of HP turbine
    • doi:10.1006/jfls.1999.0254
    • Vahdati, M., Sayma, A. I. & Imregun, M. 2000 Multi-stage whole-annulus forced response predictions using an integrated non-linear analysis technique - part II: study of HP turbine. J. Fluid Struct. 14, 103-125. (doi:10.1006/jfls.1999.0254)
    • (2000) J. Fluid Struct , vol.14 , pp. 103-125
    • Vahdati, M.1    Sayma, A.I.2    Imregun, M.3
  • 117
  • 118
    • 0036493824 scopus 로고    scopus 로고
    • Computational study of intake duct effects on fan flutter stability
    • Vahdati, M., Bréard, C., Sayma, A. I. & Imregun, M. 2002 Computational study of intake duct effects on fan flutter stability. AIAA J. 40, 408-418.
    • (2002) AIAA J , vol.40 , pp. 408-418
    • Vahdati, M.1    Bréard, C.2    Sayma, A.I.3    Imregun, M.4
  • 119
    • 0021623457 scopus 로고
    • A linearized unsteady aerodynamic analysis for transonic cascades
    • doi:10.1017/S002211208400272X
    • Verdon, J. M. & Caspar, J. R. 1984 A linearized unsteady aerodynamic analysis for transonic cascades. J. Fluid Mech. 149, 403-429. (doi:10.1017/S002211208400272X)
    • (1984) J. Fluid Mech , vol.149 , pp. 403-429
    • Verdon, J.M.1    Caspar, J.R.2
  • 120
    • 0036870362 scopus 로고    scopus 로고
    • Navier-Stokes solvers in European aircraft design
    • doi: 10.1016/80376-0421(02)00050-7
    • Voss, J. B., Rizzi, A., Darracq, D. & Hirshel, E. H. 2002 Navier-Stokes solvers in European aircraft design. Prog. Aerosp. Sci. 38, 601-697. (doi: 10.1016/80376-0421(02)00050-7)
    • (2002) Prog. Aerosp. Sci , vol.38 , pp. 601-697
    • Voss, J.B.1    Rizzi, A.2    Darracq, D.3    Hirshel, E.H.4
  • 121
    • 85040284723 scopus 로고
    • The calculation of steady and unsteady transonic flow in cascades
    • 118, University of Cambridge
    • Whitehead, D. S. 1982 The calculation of steady and unsteady transonic flow in cascades. Department of Engineering Report CUED/A-Turbo/TR 118, University of Cambridge.
    • (1982) Department of Engineering Report CUED/A-Turbo/TR
    • Whitehead, D.S.1
  • 122
    • 32044473950 scopus 로고    scopus 로고
    • The effect of stagger variability in gas turbine fan assemblies
    • Institution of Mechanical Engineers, pp
    • Wilson, M. J., Imregun, M. & Sayma, A. I. 2005 The effect of stagger variability in gas turbine fan assemblies. In Int. Conf. on Compressors and their Systems. Institution of Mechanical Engineers, pp. 507-515.
    • (2005) Int. Conf. on Compressors and their Systems , pp. 507-515
    • Wilson, M.J.1    Imregun, M.2    Sayma, A.I.3
  • 123
    • 33750812462 scopus 로고    scopus 로고
    • The effect of stagger variability in gas turbine fan assemblies
    • GT2006-90434
    • Wilson, M. J., Imregun, M. & Sayma, A. I. 2006 The effect of stagger variability in gas turbine fan assemblies. ASME Turbo Exp. GT2006-90434.
    • (2006) ASME Turbo Exp
    • Wilson, M.J.1    Imregun, M.2    Sayma, A.I.3
  • 124
    • 20444502508 scopus 로고    scopus 로고
    • Whole-annulus aeroelasticity analysis of a 17-bladerow WRF compressor using an unstructured Navier-stokes solver
    • doi:10.1080/10618560410001715554
    • Wu, X., Vahdati, M., Sayma, A. I. & Imregun, M. 2005 Whole-annulus aeroelasticity analysis of a 17-bladerow WRF compressor using an unstructured Navier-stokes solver. Int. J. Comput. Fluid Dyn. 19, 211-223. (doi:10.1080/10618560410001715554)
    • (2005) Int. J. Comput. Fluid Dyn , vol.19 , pp. 211-223
    • Wu, X.1    Vahdati, M.2    Sayma, A.I.3    Imregun, M.4
  • 126
    • 0242273162 scopus 로고    scopus 로고
    • Status of unsteady aerodynamic prediction for flutter of high-performance aircraft
    • Yurkovich, R. 2003 Status of unsteady aerodynamic prediction for flutter of high-performance aircraft. J. Aircraft 40, 832-842.
    • (2003) J. Aircraft , vol.40 , pp. 832-842
    • Yurkovich, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.