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Vortex mixing for supersonic combustion
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Experimental study of the effect of streamwise vorticity on supersonic mixing enhancement
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Near-field flow of supersonic swirling jets
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Effect of shock strength on oblique shock-wave/vortex interaction
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Computational study of the flowfields associated with oblique shock/vortex interactions
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Progress toward shock enhancement of supersonic combustion processes
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A systematic experimental and computational investigation of a class of contoured wall fuel injectors
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Low angle injection into a supersonic flow
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Three-dimensional computation of parallel and non-parallel injection in supersonic flow
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Summary of GASP code applications and evaluation effort for scramjet combustor flowfields
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Nedungadi, A., "A Computational Study of Oblique Shock/Vortex Interactions and Its Application for Supersonic Mixing Enhancement," Ph.D. Dissertation, Dept. Aerospace Engineering, Univ. of Maryland, College Park, MD, May 1997.
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A numerical study of fuel mixing enhancement using an oblique shock/vortex interaction
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Nedungadi, A., and Lewis, M. J., "A Numerical Study of Fuel Mixing Enhancement Using an Oblique Shock/Vortex Interaction," AIAA Paper 96-2920, July 1996.
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