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Volumn 42, Issue 1, 2005, Pages 38-44

Jet interaction in supersonic flow with a downstream surface ramp

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; JETS; PARAMETER ESTIMATION; TURBULENCE; VISCOSITY;

EID: 14544271556     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.4021     Document Type: Article
Times cited : (7)

References (16)
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    • Jacobsen, L.1    Gallimore, S.2    Schetz, J.3    O'Brien, W.4
  • 2
    • 14544290891 scopus 로고    scopus 로고
    • Numerical studies of the jet interaction flowfleld with a main jet and an array of smaller jets
    • Paper 2002-4.7.1, Sept.
    • Viti, V., Schetz, J., and Neel, R., "Numerical Studies of the Jet Interaction Flowfleld with a Main Jet and an Array of Smaller Jets," International Congress of Aeronautical Sciences, Paper 2002-4.7.1, Sept. 2002.
    • (2002) International Congress of Aeronautical Sciences
    • Viti, V.1    Schetz, J.2    Neel, R.3
  • 4
    • 3343005389 scopus 로고    scopus 로고
    • A comparison of turbulence models for a supersonic jet in transonic cross flow
    • Jan.
    • Payne, J. L., Roy, C. J., and Beresh, S. J., "A Comparison of Turbulence Models for a Supersonic Jet in Transonic Cross Flow," AIAA Paper 2001-1048, Jan. 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.1048
    • Payne, J.L.1    Roy, C.J.2    Beresh, S.J.3
  • 5
    • 0027640966 scopus 로고
    • Comparison of two-equation turbulence models for boundary layers with pressure gradient
    • Wilcox, D. C., "Comparison of Two-Equation Turbulence Models for Boundary Layers with Pressure Gradient," AIAA Journal, Vol. 38, No. 8, 1993, pp. 1414-1421.
    • (1993) AIAA Journal , vol.38 , Issue.8 , pp. 1414-1421
    • Wilcox, D.C.1
  • 6
    • 84983127736 scopus 로고    scopus 로고
    • Parameters affecting penetration of a single jet into a supersonic crossflow: A CFD study - II
    • Jan.
    • Roger, R. P., and Chan, S. C., "Parameters Affecting Penetration of a Single Jet into a Supersonic Crossflow: A CFD Study - II," AIAA Paper 98-0425, Jan. 1998.
    • (1998) AIAA Paper , vol.98 , Issue.425
    • Roger, R.P.1    Chan, S.C.2
  • 7
    • 14544305423 scopus 로고    scopus 로고
    • A numerical study of fuel mixing enhancement using oblique shock/vortex interactions
    • Feb.
    • Nedungadi, A., and Lewis, M. J., "A Numerical Study of Fuel Mixing Enhancement Using Oblique Shock/Vortex Interactions," AIAA Paper 96-2920, Feb. 1997.
    • (1997) AIAA Paper , vol.96 , Issue.2920
    • Nedungadi, A.1    Lewis, M.J.2
  • 8
    • 3342922466 scopus 로고    scopus 로고
    • Analysis of the scaling effects for missile configuration with lateral thruster
    • Jan.
    • Hsieh, T., "Analysis of the Scaling Effects for Missile Configuration with Lateral Thruster," AIAA Paper 99-0810, Jan. 1999.
    • (1999) AIAA Paper , vol.99 , Issue.810
    • Hsieh, T.1
  • 9
    • 85086489239 scopus 로고    scopus 로고
    • Experimental and computational comparison of an underexpanded jet flowfield
    • Jan.
    • McDaniel, J., Glass, C., Staack, D., and Miller, C., "Experimental and Computational Comparison of an Underexpanded Jet Flowfield," AIAA Paper 2002-0305, Jan. 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.305
    • McDaniel, J.1    Glass, C.2    Staack, D.3    Miller, C.4
  • 10
    • 3342925991 scopus 로고    scopus 로고
    • AeroSoft, Inc., Blacksburg, VA
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  • 11
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  • 12
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    • Blunt-body flow simulations
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  • 14
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  • 16
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    • Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at mach 2.92 to 6.4
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    • (1961) NASA TN D-580
    • Cubbison, R.W.1    Anderson, B.H.2    Ward, J.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.