메뉴 건너뛰기




Volumn 85, Issue 11-14, 2007, Pages 818-832

Application of Navier-Stokes simulations for aeroelastic stability assessment in transonic regime

Author keywords

Aeroelasticity; Fluid structure interface; Flutter; Grid deformation; Navier Stokes equations; ROMs; Transonic regime

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; EULER EQUATIONS; FLUID STRUCTURE INTERACTION; NAVIER STOKES EQUATIONS;

EID: 34248208696     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2007.01.005     Document Type: Article
Times cited : (66)

References (46)
  • 1
    • 0018493237 scopus 로고
    • On the transonic-dip mechanism of flutter of a sweptback wing
    • Isogai K. On the transonic-dip mechanism of flutter of a sweptback wing. AIAA J 17 (1979) 735-795
    • (1979) AIAA J , vol.17 , pp. 735-795
    • Isogai, K.1
  • 2
    • 0242304914 scopus 로고    scopus 로고
    • Computational aeroelasticity: success, progress, challenge
    • Schuster D.M., Liu D.D., and Huttsell L.J. Computational aeroelasticity: success, progress, challenge. J Aircraft 40 5 (2003) 843-856
    • (2003) J Aircraft , vol.40 , Issue.5 , pp. 843-856
    • Schuster, D.M.1    Liu, D.D.2    Huttsell, L.J.3
  • 3
    • 0242273162 scopus 로고    scopus 로고
    • Status of unsteady aerodynamic prediction for flutter of high-performance aircraft
    • Yurkovich R. Status of unsteady aerodynamic prediction for flutter of high-performance aircraft. J Aircraft 40 5 (2003) 832-842
    • (2003) J Aircraft , vol.40 , Issue.5 , pp. 832-842
    • Yurkovich, R.1
  • 4
    • 34248150382 scopus 로고    scopus 로고
    • Lee-Raush EM, Batina JT, Wing flutter boundary prediction using unsteady Euler aerodynamic method. AIAA Paper 93-1422, April; 1993.
  • 5
    • 84959324234 scopus 로고    scopus 로고
    • Bennet RM, Edwards JW. An overview of recent developments in computational aeroelasticity. In: Proceedings of the 29th AIAA fluid dynamics conference, Albuquerque, NM; 1998.
  • 6
    • 15344349684 scopus 로고    scopus 로고
    • Fluid-structure interaction for aeroelastic applications
    • Kamakoti R., and Shyy W. Fluid-structure interaction for aeroelastic applications. Prog Aerospace Sci 40 8 (2004) 535-558
    • (2004) Prog Aerospace Sci , vol.40 , Issue.8 , pp. 535-558
    • Kamakoti, R.1    Shyy, W.2
  • 7
    • 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
    • Farhat C., Geuzaine P., and Brown G. Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter. Comput Fluids 32 (2003) 3-29
    • (2003) Comput Fluids , vol.32 , pp. 3-29
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3
  • 8
    • 34248159961 scopus 로고    scopus 로고
    • Melville R. Nonlinear mechanisms of aeroelastic instability for the F-16. AIAA Paper 2002-0871, January; 2002.
  • 9
    • 32044458550 scopus 로고    scopus 로고
    • Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
    • Farhat C., van der Zee K.G., and Geuzaine P. Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity. Comput Meth Appl Mech Eng 195 17-18 (2006) 1973-2001
    • (2006) Comput Meth Appl Mech Eng , vol.195 , Issue.17-18 , pp. 1973-2001
    • Farhat, C.1    van der Zee, K.G.2    Geuzaine, P.3
  • 10
    • 0037401453 scopus 로고    scopus 로고
    • FSI analysis in supersonic fluid flow
    • Kroyer R. FSI analysis in supersonic fluid flow. Comput Struct 72 (2003) 755-764
    • (2003) Comput Struct , vol.72 , pp. 755-764
    • Kroyer, R.1
  • 11
    • 0032667945 scopus 로고    scopus 로고
    • Finite element analysis of fluid flows fully coupled with structural interactions
    • Bathe K.-J., Zhang H., and Ji S. Finite element analysis of fluid flows fully coupled with structural interactions. Comput Struct 72 (1999) 1-16
    • (1999) Comput Struct , vol.72 , pp. 1-16
    • Bathe, K.-J.1    Zhang, H.2    Ji, S.3
  • 12
    • 0035793736 scopus 로고    scopus 로고
    • Fluid structure interaction with large structural displacements
    • Le Tallec P., and Mouro J. Fluid structure interaction with large structural displacements. Comput Meth Appl Mech Eng 190 (2001) 3039-3067
    • (2001) Comput Meth Appl Mech Eng , vol.190 , pp. 3039-3067
    • Le Tallec, P.1    Mouro, J.2
  • 13
    • 2342565951 scopus 로고    scopus 로고
    • Finite element developments for general fluid flows with structural interactions
    • Bathe K.-J., and Zhang H. Finite element developments for general fluid flows with structural interactions. Int J Numer Meth Eng 60 (2004) 213-232
    • (2004) Int J Numer Meth Eng , vol.60 , pp. 213-232
    • Bathe, K.-J.1    Zhang, H.2
  • 14
    • 34248212720 scopus 로고    scopus 로고
    • Preliminary assessment of the complete aeroelastic simulation of the M-346 in transonic condition with a CFD Navier-Stokes solver
    • Cavagna L., Quaranta G., Mantegazza P., Merlo E., Marchetti D., and Martegani M. Preliminary assessment of the complete aeroelastic simulation of the M-346 in transonic condition with a CFD Navier-Stokes solver. Aerotec Missili Spaz 84 3 (2005) 115-127
    • (2005) Aerotec Missili Spaz , vol.84 , Issue.3 , pp. 115-127
    • Cavagna, L.1    Quaranta, G.2    Mantegazza, P.3    Merlo, E.4    Marchetti, D.5    Martegani, M.6
  • 15
    • 0025475785 scopus 로고
    • Unsteady Euler airfoil solution using unstructured dynamic meshes
    • Batina J. Unsteady Euler airfoil solution using unstructured dynamic meshes. AIAA J 28 (1990) 1381-1388
    • (1990) AIAA J , vol.28 , pp. 1381-1388
    • Batina, J.1
  • 16
    • 0036465944 scopus 로고    scopus 로고
    • A three-dimensional torsional spring analogy method for unstructured dynamic meshes
    • Degand C., and Farhat C. A three-dimensional torsional spring analogy method for unstructured dynamic meshes. Comput Struct 80 (2002) 305-316
    • (2002) Comput Struct , vol.80 , pp. 305-316
    • Degand, C.1    Farhat, C.2
  • 17
    • 34248160461 scopus 로고    scopus 로고
    • Byun C, Guruswamy G. A parallel, multi-block, moving grid method for aeroelastic applications on full aircraft. AIAA Paper 98-4782, September; 1998.
  • 18
    • 0020860514 scopus 로고
    • Arbitrary Lagrangian-Eulerian finite element methods
    • Belytschko T., and Hughes T.J. (Eds), Elsevier, Amsterdam, The Netherlands [chapter 10]
    • Donea J. Arbitrary Lagrangian-Eulerian finite element methods. In: Belytschko T., and Hughes T.J. (Eds). Computational methods for transient analysis (1983), Elsevier, Amsterdam, The Netherlands 474-516 [chapter 10]
    • (1983) Computational methods for transient analysis , pp. 474-516
    • Donea, J.1
  • 19
    • 34248231227 scopus 로고    scopus 로고
    • Yates EC. AGARD standard aeroelastic configurations for dynamic response. I wing 445.6 R 765, AGARD; 1985.
  • 20
    • 20044374732 scopus 로고    scopus 로고
    • Computational-fluid-dynamic-based aeroelastic analysis and structural design optimization - a researcher's perspective
    • Raveh D.E. Computational-fluid-dynamic-based aeroelastic analysis and structural design optimization - a researcher's perspective. Comput Meth Appl Mech Eng 194 (2005) 3453-3471
    • (2005) Comput Meth Appl Mech Eng , vol.194 , pp. 3453-3471
    • Raveh, D.E.1
  • 21
    • 34248189652 scopus 로고    scopus 로고
    • Cavagna L, Quaranta G, Ghiringhelli GL, Mantegazza P. Efficient application of CFD aeroelastic methods using commercial software. In: International forum on aeroelasticity and structural dynamics IFASD-2005, Munich, Germany; 2005.
  • 22
    • 33749254670 scopus 로고    scopus 로고
    • An investigation over CFD based models for the identification of nonlinear unsteady aerodynamics responses
    • Lisandrin P., Carpentieri G., and Van Tooren M. An investigation over CFD based models for the identification of nonlinear unsteady aerodynamics responses. AIAA J 44 9 (2006) 2043-2050
    • (2006) AIAA J , vol.44 , Issue.9 , pp. 2043-2050
    • Lisandrin, P.1    Carpentieri, G.2    Van Tooren, M.3
  • 23
    • 34248213594 scopus 로고    scopus 로고
    • Giavotto V, Mantegazza P, Otto LD, Lucchesini M, Mantelli R. Fast flutter clearance by parameter variation. CP 354, AGARD, September; 1983.
  • 24
    • 34248177823 scopus 로고    scopus 로고
    • Scotti A, Quaranta G, Ricci S. Active control of three surface wind tunnel aeroelastic demonstrator: Modelling and correlation. In: International forum on aeroelasticity and structural dynamics IFASD-2005, Munich, Germany; 2005.
  • 25
    • 0025433472 scopus 로고
    • Reduced order aeroelastic models via dynamic residualization
    • Karpel M. Reduced order aeroelastic models via dynamic residualization. J Aircraft 27 5 (1990) 449-455
    • (1990) J Aircraft , vol.27 , Issue.5 , pp. 449-455
    • Karpel, M.1
  • 27
    • 0032649041 scopus 로고    scopus 로고
    • Single finite states modeling of aerodynamic forces related to structural motions and gusts
    • Pasinetti G., and Mantegazza P. Single finite states modeling of aerodynamic forces related to structural motions and gusts. AIAA J 37 5 (1999) 604-612
    • (1999) AIAA J , vol.37 , Issue.5 , pp. 604-612
    • Pasinetti, G.1    Mantegazza, P.2
  • 29
    • 0014779865 scopus 로고
    • Application of oscillatory aerodynamic theory to estimation of stability derivatives
    • Rodden W., and Gesling J. Application of oscillatory aerodynamic theory to estimation of stability derivatives. J Aircraft 7 3 (1970) 272-275
    • (1970) J Aircraft , vol.7 , Issue.3 , pp. 272-275
    • Rodden, W.1    Gesling, J.2
  • 30
    • 0034999906 scopus 로고    scopus 로고
    • Thomas JP, Dowell EH, Hall KC. Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models. In: Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference and exhibit, Seattle (WA); 2001, also published in J Aircraft 40 (2003).
  • 31
    • 0034140207 scopus 로고    scopus 로고
    • Two efficient staggered algorithms for the serial and parallel solution of three-dimensional nonlinear transient aeroelastic problems
    • Farhat C., and Lesoinne M. Two efficient staggered algorithms for the serial and parallel solution of three-dimensional nonlinear transient aeroelastic problems. Comput Meth Appl Mech Eng 182 (2000) 499-515
    • (2000) Comput Meth Appl Mech Eng , vol.182 , pp. 499-515
    • Farhat, C.1    Lesoinne, M.2
  • 32
    • 0033873883 scopus 로고    scopus 로고
    • Evaluation of computational algorithms for suitable fluid-structure interactions
    • Smith M.J., Hodges D.H., and Cesnik C.E. Evaluation of computational algorithms for suitable fluid-structure interactions. J Aircraft 37 2 (2000) 282-294
    • (2000) J Aircraft , vol.37 , Issue.2 , pp. 282-294
    • Smith, M.J.1    Hodges, D.H.2    Cesnik, C.E.3
  • 33
    • 0029256189 scopus 로고
    • Matching fluid and structure meshes for aeroelastic computations: a parallel approach
    • Maman N., and Farhat C. Matching fluid and structure meshes for aeroelastic computations: a parallel approach. Comput Struct 54 4 (1995) 779-785
    • (1995) Comput Struct , vol.54 , Issue.4 , pp. 779-785
    • Maman, N.1    Farhat, C.2
  • 34
    • 84966237423 scopus 로고
    • Surfaces generated by moving least squares methods
    • Lancaster P., and Salkauskas K. Surfaces generated by moving least squares methods. Math Comput 37 (1981) 141-158
    • (1981) Math Comput , vol.37 , pp. 141-158
    • Lancaster, P.1    Salkauskas, K.2
  • 35
    • 34248188643 scopus 로고    scopus 로고
    • Schaback R. Remarks on meshless local construction of surfaces. In: Proceedings of IMA mathematics of surfaces IX conference, Cambridge; 2000.
  • 36
    • 0346847275 scopus 로고
    • Piecewise polynomial, positive definite and compactly supported radial functions of minimal degree
    • Wendland H. Piecewise polynomial, positive definite and compactly supported radial functions of minimal degree. Adv Comput Math 4 (1995) 389-396
    • (1995) Adv Comput Math , vol.4 , pp. 389-396
    • Wendland, H.1
  • 38
    • 34248163929 scopus 로고    scopus 로고
    • Quaranta G, Masarati P, Mantegazza P. A conservative mesh-free approach for fluid-structure interface problems. In: Papadrakakis M, Oñate E, Schrefler B, editors. International conference on computational methods for coupled problems in science and engineering, CIMNE, Santorini, Greece; 2005.
  • 39
    • 0036093649 scopus 로고    scopus 로고
    • A procedure for tetrahedral boundary layer mesh generation
    • Bottasso C.L., and Detomi D. A procedure for tetrahedral boundary layer mesh generation. Eng Comput 18 1 (2002) 66-79
    • (2002) Eng Comput , vol.18 , Issue.1 , pp. 66-79
    • Bottasso, C.L.1    Detomi, D.2
  • 41
    • 34248181544 scopus 로고    scopus 로고
    • Venkatakrishnan V, Mavriplis DJ. Agglomeration multigrid for the three-dimensional Euler equations. AIAA Paper 94-0069; 1994.
  • 42
    • 34248173906 scopus 로고    scopus 로고
    • Ollivier-Gooch C. Robust coarsening of unstructured meshes for multigrid methods. In: Proceedings of the 14th AIAA computational fluid dynamics conference, Norfolk (VA); 1999.
  • 43
    • 34248175232 scopus 로고    scopus 로고
    • Fluent 6.1 user's guide; 2003.
  • 44
    • 0031124847 scopus 로고    scopus 로고
    • Stability and accuracy of numerical boundary conditions in aeroelastic analysis
    • Giles M.B. Stability and accuracy of numerical boundary conditions in aeroelastic analysis. Int J Numer Meth Fluids 24 8 (1997) 739-757
    • (1997) Int J Numer Meth Fluids , vol.24 , Issue.8 , pp. 739-757
    • Giles, M.B.1
  • 45
    • 0030289123 scopus 로고    scopus 로고
    • Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations
    • Lee-Rausch E.M., and Batina J.T. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations. J Aircraft 33 6 (1996) 1139-1147
    • (1996) J Aircraft , vol.33 , Issue.6 , pp. 1139-1147
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 46
    • 0022061983 scopus 로고
    • A harmonic gradient method for unsteady supersonic flow calculations
    • Chen P.C., and Liu D.D. A harmonic gradient method for unsteady supersonic flow calculations. J Aircraft 22 15 (1985) 371-379
    • (1985) J Aircraft , vol.22 , Issue.15 , pp. 371-379
    • Chen, P.C.1    Liu, D.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.