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Volumn 9, Issue , 2007, Pages 5960-5991

F- 16XL unsteady simulations for the CAWAPI facet of RTO task group AVT-113

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT TEST PROGRAM; SIDESLIPS; SURFACE PRESSURE COEFFICIENT; SYMMETRIC CONDITION;

EID: 34250880816     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (38)

References (20)
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    • Hummel, D., and Redeker, G., A new vortex flow experiment for computer code validation. Presented at RTO AVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper Number 8, in Loen Norway during May 7-11, 2001.
    • Hummel, D., and Redeker, G., "A new vortex flow experiment for computer code validation. Presented at RTO AVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper Number 8, in Loen Norway during May 7-11, 2001.
  • 6
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    • Detached-Eddy Simulation with Compressibility Corrections Applied to a Supersonic Axisymmetric Base
    • Forsythe, J.R., Hoffmann, K.A., Cummings, R.M., and Squires, K.D., "Detached-Eddy Simulation with Compressibility Corrections Applied to a Supersonic Axisymmetric Base," Journal of Fluids Engineering, Vol. 124, No. 4, 2002, pp. 911-923.
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    • Forsythe, J.R.1    Hoffmann, K.A.2    Cummings, R.M.3    Squires, K.D.4
  • 7
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    • Detached-Eddy Simulations and Reynolds-Averaged Navier-Stokes Simulations of Delta Wing Vortical Flowfields
    • Morton, S.A., Forsythe, J.R., Mitchell, A.M., and Hajek, D., "Detached-Eddy Simulations and Reynolds-Averaged Navier-Stokes Simulations of Delta Wing Vortical Flowfields," Journal of Fluids Engineering, Vol. 124, No. 4, 2002, pp. 924-932.
    • (2002) Journal of Fluids Engineering , vol.124 , Issue.4 , pp. 924-932
    • Morton, S.A.1    Forsythe, J.R.2    Mitchell, A.M.3    Hajek, D.4
  • 8
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    • Analysis of Delta-Wing Vortical Substructures Using Detached-Eddy Simulation
    • Mitchell, A.M., Morton, S.A., Forsythe, J.R., and Cummings, R.M., "Analysis of Delta-Wing Vortical Substructures Using Detached-Eddy Simulation," AIAA Journal, Vol. 44, No 5, 2006, pp. 964-972.
    • (2006) AIAA Journal , vol.44 , Issue.5 , pp. 964-972
    • Mitchell, A.M.1    Morton, S.A.2    Forsythe, J.R.3    Cummings, R.M.4
  • 9
    • 2342452531 scopus 로고    scopus 로고
    • Detached-Eddy Simulation of Fighter Aircraft at High Alpha
    • Forsythe, J.R., Squires, K.D., Wurtzler, K.E., and Spalart, P.R., "Detached-Eddy Simulation of Fighter Aircraft at High Alpha," Journal of Aircraft, Vol. 41, No. 2, 2004, pp. 193-200.
    • (2004) Journal of Aircraft , vol.41 , Issue.2 , pp. 193-200
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  • 10
    • 22544439693 scopus 로고    scopus 로고
    • Unsteady Computations of Abrupt Wing Stall Using Detached-Eddy Simulation
    • Forsythe, J.R., and Woodson, S.H., "Unsteady Computations of Abrupt Wing Stall Using Detached-Eddy Simulation," Journal of Aircraft, Vol. 42, No. 3,2005, pp. 606-616.
    • (2005) Journal of Aircraft , vol.42 , Issue.3 , pp. 606-616
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  • 11
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    • AIAA Paper 2004-1676, April
    • Morton, S.A., Cummings, R.M., and Kholodar, D.B., "High Resolution Turbulence Treatment of F/A-18 Tail Buffet," AIAA Paper 2004-1676, April 2004.
    • (2004)
    • Morton, S.A.1    Cummings, R.M.2    Kholodar, D.B.3
  • 13
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    • Cobalt: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Solver
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    • (1998) Adv. Eng. Software , vol.29 , Issue.3-6 , pp. 365-373
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  • 14
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    • G. Karypis, K. Schloegel, and V. Kumar, "Parmetis: Parallel Graph Partitioning and Sparse Matrix Ordering Library, Version 3.1," Technical report, Dept. Computer Science, University of Minnesota, 2003.
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  • 18
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    • Gursul, I.1
  • 19
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.