Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil von Pruski, B. J, Bowersox, R. D. W

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Response of a hypersonic turbulent boundary layer to favourable pressure gradients von Tichenor, N. R., Humble, R. A., Bowersox, R. D. W.

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A method to analyze molecular tagging velocimetry data using the Hough transform von Sanchez-Gonzalez, R, McManamen, B, Bowersox, R D W, North, S W

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Crosshatch roughness distortions on a hypersonic turbulent boundary layer von Peltier, S. J., Humble, R. A., Bowersox, R. D. W.

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Visualization of the structural response of a hypersonic turbulent boundary layer to convex curvature von HUMBLE, R. A, PELTIER, S. J, BOWERSOX, R. D. W

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Jet Interaction with a Primary Jet and an Array of Smaller Jets von Viti, Valerio, Wallis, Scott, Schetz, Joseph A, Neel, Reece, Bowersox, R. D. W

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Low-temperature collisional quenching of NO A2Σ+(v′ = 0) by NO(X2Π) and O2 between 34 and 109 K von Sánchez-González, R., Eveland, W. D., West, N. A., Mai, C. L. N., Bowersox, R. D. W., North, S. W.

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Velocity and temperature fluctuations in a high-speed shock–turbulence interaction von McManamen, B., Donzis, D.A., North, S.W., Bowersox, R.D.W.

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Experimental Investigation of the Flow Structure Near a Single Wraparound Fin von Tilmann, C. P, Huffman, R. E, Buter, T. A, Bowersox, R. D. W

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Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers von Bowersox, R. D. W, Wier, R. C, Glawe, D. D, Gogineni, S

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Characterization of the Flowfield near a Wrap-Around Fin at Mach 2.8 von Tilmann, C. P, Buter, T. A, Bowersox, R. D. W

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Low-temperature collisional quenching of NO A{sup 2}Σ{sup +}(v′ = 0) by NO(X{sup 2}Π) and O{sub 2} between 34 and 109 K von Sánchez-González, R., Eveland, W. D., West, N. A., North, S. W., Mai, C. L. N., Bowersox, R. D. W.

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Performance characterization of a highly offset diffuser with vortex generator jets von Senseney, M. B, Buter, T. A, Bowersox, R. D. W

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Numerical Investigation of Supersonic Injection Using a Reynolds-Stress Turbulence Model von Chenault, Clarence F, Beran, Philip S, Bowersox, Rodney D. W

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Influence of Curvature-Driven Favorable Pressure Gradient on Supersonic Turbulent Boundary Layer von Luker, Joel J, Bowersox, Rodney D. W, Buter, Thomas A

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Temporal Turbulent Flow Structure for Supersonic Rough-Wall Boundary Layers von Latin, Robert M, Bowersox, Rodney D. W

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Low-temperature collisional quenching of NO A(2)Σ(+)(v' = 0) by NO(X(2)Π) and O2 between 34 and 109 K von Sánchez-González, R, Eveland, W D, West, N A, Mai, C L N, Bowersox, R D W, North, S W

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Experimental investigation of supersonic gaseous injection into a supersonic freestream von McCann, Gregory J, Bowersox, Rodney D. W

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Sonic Boom Alleviation Using Keel Configurations von Marconi, Frank, Bowersox, Rodney D. W, Schetz, Joseph A

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Combined laser Doppler velocimetry and cross-wire anemometry analysis for supersonic turbulent flow von Bowersox, Rodney D. W

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