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Volumn , Issue , 1996, Pages 1-14

Considerations in the comparison of experimental data with simulations - Consistency of math models and flow physics

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; WALL FLOW;

EID: 84894517235     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2030     Document Type: Conference Paper
Times cited : (2)

References (25)
  • 2
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    • Jameson, A., "Universities Foster CFD Growth," Aerospace America, Feb. 1992, pp. 42-47.
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    • Jameson, A.1
  • 5
    • 4243239392 scopus 로고
    • Prediction of Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows
    • AIAA Paper 87-1367, Jun. 8-10, Honolulu, HI
    • Horstman, C. C., "Prediction of Hypersonic Shock Wave/Turbulent Boundary Layer Interaction Flows," AIAA Paper 87-1367, AIAA 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Jun. 8-10, 1987, Honolulu, HI.
    • (1987) AIAA 19Th Fluid Dynamics, Plasma Dynamics and Lasers Conference
    • Horstman, C.C.1
  • 8
    • 0018504419 scopus 로고
    • Comparison of Multi-Equation Turbulence Models for Several Shock Boundary Layer Interaction Flows
    • Viegas, J. R., and Horstman, C. C., "Comparison of Multi-Equation Turbulence Models for Several Shock Boundary Layer Interaction Flows," AIAA Journal, Vol. 17, No. 8, 1979, pp. 811-820.
    • (1979) AIAA Journal , vol.17 , Issue.8 , pp. 811-820
    • Viegas, J.R.1    Horstman, C.C.2
  • 11
    • 0025462835 scopus 로고
    • Supersonic Compression Corner Applications of a Multi-Scale Model for Turbulent Flows
    • Jul
    • Wilcox, D. D., "Supersonic Compression Corner Applications of a Multi-Scale Model for Turbulent Flows," AIAA Journal, Vol. 78, No. 7, Jul. 1990, pp. 1194-1198.
    • (1990) AIAA Journal , vol.78 , Issue.7 , pp. 1194-1198
    • Wilcox, D.D.1
  • 14
    • 0020944128 scopus 로고
    • Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield
    • Dolling, D. S., and Murphy, M. T., "Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield," AIAA Journal, Vol. 21, Dec. 1983, pp. 1628-1634.
    • (1983) AIAA Journal , vol.21 , pp. 1628-1634
    • Dolling, D.S.1    Murphy, M.T.2
  • 16
    • 0026156652 scopus 로고    scopus 로고
    • Separation Shock Motion and Ensemble-Averaged Wall Pressures in a Mach 5 Compression Ramp Interaction
    • May 1991
    • Erengil, M. E., and Dolling, D. S., "Separation Shock Motion and Ensemble-Averaged Wall Pressures in a Mach 5 Compression Ramp Interaction," AIAA Journal, Vol. 29, No. 5, May 1991, pp. 728-735.
    • AIAA Journal , vol.29 , Issue.5 , pp. 728-735
    • Erengil, M.E.1    Dolling, D.S.2
  • 17
    • 0025447238 scopus 로고
    • Detection of Turbulent Boundary Layer Separation Using Fluctuating Wall Pressure Signals
    • Jun
    • Gramann, R. A., and Dolling, D. S., "Detection of Turbulent Boundary Layer Separation Using Fluctuating Wall Pressure Signals," AIAA Journal, Vol. 28, No. 6, Jun. 1990, pp. 1052-1056.
    • (1990) AIAA Journal , vol.28 , Issue.6 , pp. 1052-1056
    • Gramann, R.A.1    Dolling, D.S.2
  • 18
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    • Interpretation of Separation Lines from Surface Tracers in Shock Induced Turbulent Flow
    • Gramann, R. A., and Dolling, D. S., "Interpretation of Separation Lines from Surface Tracers in Shock Induced Turbulent Flow," AIAA Journal, Vol. 25, No. 12, 1987, pp. 1545-1546.
    • (1987) AIAA Journal , vol.25 , Issue.12 , pp. 1545-1546
    • Gramann, R.A.1    Dolling, D.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.