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Volumn , Issue , 2009, Pages

Effects of fuel slosh on flutter prediction

Author keywords

[No Author keywords available]

Indexed keywords

AVIATION; COMPUTATIONAL FLUID DYNAMICS; DESIGN AIDS; FLUID STRUCTURE INTERACTION; FLUTTER (AERODYNAMICS); FUELS; STRUCTURAL DYNAMICS;

EID: 84855633247     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-2682     Document Type: Conference Paper
Times cited : (14)

References (14)
  • 1
    • 84964311108 scopus 로고    scopus 로고
    • F-16 limit cycle oscillation testing with asymmetric store
    • AIAA-1999-3142, Norfolk, Virginia
    • Dawson, K.S. and Sussingham J.C., "F-16 Limit Cycle Oscillation Testing with Asymmetric Store", AIAA-1999-3142, AIAA Applied Aerodynamics Conference, 17th, Norfolk, Virginia, 1999.
    • (1999) AIAA Applied Aerodynamics Conference, 17th
    • Dawson, K.S.1    Sussingham, J.C.2
  • 2
    • 84896856632 scopus 로고    scopus 로고
    • Accelerated flutter testing: A possible technique to expedite flutter testing for new aircraft
    • AIAA- 2004-6822, Summit, Woodland Hills, California
    • Harris, C., "Accelerated Flutter Testing: A Possible Technique to Expedite Flutter Testing for New Aircraft", AIAA- 2004-6822, USAF Developmental Test and Evaluation Summit, Woodland Hills, California, 2004.
    • (2004) USAF Developmental Test and Evaluation
    • Harris, C.1
  • 4
    • 0035793731 scopus 로고    scopus 로고
    • A linearized method for the frequency analysis of three- dimensional fluid/structure interaction problems in all flow regimes
    • Lesoinne, M., Sarkis, M., Hetmaniuk, U., and Farhat, C., "A Linearized Method for the Frequency Analysis of Three- Dimensional Fluid/Structure Interaction Problems in All Flow Regimes", Computer Methods in Applied Mechanics and Engineering, Vol. 190, 2001, pp. 3121-3146.
    • (2001) Computer Methods in Applied Mechanics and Engineering , vol.190 , pp. 3121-3146
    • Lesoinne, M.1    Sarkis, M.2    Hetmaniuk, U.3    Farhat, C.4
  • 5
    • 0035390399 scopus 로고    scopus 로고
    • A CFD based method for solving aeroelastic eigenproblems in the subsonic, transonic, and supersonic regimes
    • Lesoinne, M., and Farhat, C., "A CFD Based Method for Solving Aeroelastic Eigenproblems in the Subsonic, Transonic, and Supersonic Regimes", AIAA Journal of Aircraft, Vol. 38, 2001, pp. 628-635.
    • (2001) AIAA Journal of Aircraft , vol.38 , pp. 628-635
    • Lesoinne, M.1    Farhat, C.2
  • 6
    • 0029138959 scopus 로고
    • Mixed explicit/implicit time integration of coupled aeroelastic problems: Three-field formulation, geometric conservation and distributed solution
    • Farhat, C., Lesoinne, M., and Maman, N., "Mixed Explicit/Implicit Time Integration of Coupled Aeroelastic Problems: Three-Field Formulation, Geometric Conservation and Distributed Solution", International Journal in Numerical Methods in Fluids, Vol. 21, 1995, pp. 807-835.
    • (1995) International Journal in Numerical Methods in Fluids , vol.21 , pp. 807-835
    • Farhat, C.1    Lesoinne, M.2    Maman, N.3
  • 7
    • 84998879868 scopus 로고
    • Stability analysis of dynamic meshes for transient aeroelastic computations
    • AIAA 1993-3325, Orlando, Florida, July 6-9
    • Lesoinne, M. and Farhat, C., "Stability Analysis of Dynamic Meshes for Transient Aeroelastic Computations", AIAA 1993-3325, AIAA Computational Fluid Dynamics Conference, 11th, Orlando, Florida, July 6-9, 1993.
    • (1993) AIAA Computational Fluid Dynamics Conference, 11th
    • Lesoinne, M.1    Farhat, C.2
  • 8
    • 0032053181 scopus 로고    scopus 로고
    • Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and eneergy conservation, optimal discretization and application to aeroelasticity
    • Farhat, C., Lesoinne, M., and Tallec, P., "Load and Motion Transfer Algorithms for Fluid/Structure Interaction Problems with Non-matching Discrete Interfaces: Momentum and Eneergy Conservation, Optimal Discretization and Application to Aeroelasticity", Computational Methods in Applied Mechanical Engeering, Vol. 157, 1998, pp. 95-114.
    • (1998) Computational Methods in Applied Mechanical Engeering , vol.157 , pp. 95-114
    • Farhat, C.1    Lesoinne, M.2    Tallec, P.3
  • 9
    • 0034140207 scopus 로고    scopus 로고
    • Two efficient staggered procedures for the serial and parallel solution of three- dimensional nonlinear transient aeroelastic problems
    • Farhat, C. and Lesoinne, M., "Two Efficient Staggered Procedures for the Serial and Parallel Solution of Three- Dimensional Nonlinear Transient Aeroelastic Problems", Computer Methods in Applied Mechanics and Engineering, Vol. 182, 2000, pp. 499-516.
    • (2000) Computer Methods in Applied Mechanics and Engineering , vol.182 , pp. 499-516
    • Farhat, C.1    Lesoinne, M.2
  • 10
    • 32044458550 scopus 로고    scopus 로고
    • Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
    • Farhat, C., van der Zee, G. and Geuzaine, P., "Provably Second-Order Time-Accurate Loosely-Coupled Solution Algorithms for Transient Nonlinear Computational Aeroelasticity", Computer Methods in Applied Mechanics and Engineering, Vol. 195, 2006, pp. 1973-2001.
    • (2006) Computer Methods in Applied Mechanics and Engineering , vol.195 , pp. 1973-2001
    • Farhat, C.1    Van Der Zee, G.2    Geuzaine, P.3
  • 11
    • 0022131039 scopus 로고
    • An eigensystem realization algorithm for modal parameter identification and model reduction
    • Juang, J.-N. and Pappa, R. S., "An Eigensystem Realization Algorithm for Modal Parameter Identification and Model Reduction", Journal of Guidance, Control, and Dynamics, Vol. 8, 1985, pp. 620-627.
    • (1985) Journal of Guidance, Control, and Dynamics , vol.8 , pp. 620-627
    • Juang, J.-N.1    Pappa, R.S.2
  • 12
    • 0037345147 scopus 로고    scopus 로고
    • Aeroelastic dynamic analysis of a full F-16 configuration for various flight conditions
    • Geuzaine, P., Brown, G., Harris, C. and Farhat, C., "Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions", AIAA Journal, Vol. 41, 2003, pp. 363-371.
    • (2003) AIAA Journal , vol.41 , pp. 363-371
    • Geuzaine, P.1    Brown, G.2    Harris, C.3    Farhat, C.4
  • 13
    • 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", Computers and Fluids, Vol. 32, 2003, pp. 3-29.
    • (2003) Computers and Fluids , vol.32 , pp. 3-29
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.