Experimental and Numerical Study of a Dual-mode Scramjet Combustor von Goyne, C. P, Rodriguez, C. G, Krauss, R. H, McDaniel, J. C, McClinton, C. R

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Preliminary X-43 flight test results von McClinton, Charles R., Rausch, Vincent L., Nguyen, Luat T., Sitz, Joel R.

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Thrust Losses in Hypersonic Engines Part 1: Methodology von Riggins, D. W, McClinton, C. R, Vitt, P. H

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Hyper-X: Foundation for future hypersonic launch vehicles von McClinton, Charles R., Rausch, Vincent L., Shaw, Robert J., Metha, Unmeel, Naftel, Chris

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X-43A Hypersonic vehicle technology development von Voland, Randall T., Huebner, Lawrence D., McClinton, Charles R.

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Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency / C.R. McClinton and G.Y. Anderson von McClinton, C. R

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Investigation of scramjet injection strategies for high Mach number flows von Riggins, D W, McClinton, C R, Rogers, R C, Bittner, R D

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Investigation of scramjet injection strategies for high Mach number flows von Riggins, D. W, McClinton, C. R, Rogers, R. C, Bittner, R. D

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Types of Alcoholic Beverages Usually Consumed by Students in 9th–12th Grades — Four States, 2005 von Roeber, J, Green, D.L, Meurer, K.M, Armitage, J.J, Maas, G.M, McClinton, R.C, Courtney, K, Cremeens, J.L, Brewer, R.D, Miller, J.W, Eaton, D

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Thrust Losses in Hypersonic Engines Part 1: Methodology von Riggins, D W, McClinton, C R, Vitt, P H

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Thrust losses in hypersonic engines. I - Methodology von Riggins, D W, McClinton, C R, Vitt, P H

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Interaction between step fuel injectors on opposite walls in a supersonic combustor model von Mcclinton, C. R.

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Effect of ratio of wall boundary layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream von Mcclinton, C. R.

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The effect of injection angle on the interaction between sonic secondary jets and a supersonic free stream von Mcclinton, C. R.

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Velocity Measurement in a Dual-Mode Supersonic Combustor using Particle Image Velocimetry von Goyne, C. P., McDaniel, J. C., Krauss, R. H., Day, S. W., Reubush, D. E., McClinton, C. R., Reubush, D. E.

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Airbreathing Hypersonic Technology Vision Vehicles and Development Dreams von McClinton, C. R., Hunt, J. L., Ricketts, R. H., Reukauf, P., Peddie, C. L.

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Evaluation of a bulk calorimeter and heat balance for determination of supersonic combustor efficiency von Mcclinton, C. R., Anderson, G. Y.

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Hyper-X Engine Design and Ground Test Program von Voland, R. T., Rock, K. E., Huebner, L. D., Witte, D. W., Fischer, K. E., McClinton, C. R.

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Normal injection of helium from swept struts into ducted supersonic flow von Mcclinton, C. R., Torrence, M. G.

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Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility von Goyne, C. P., McDaniel, J. C., Quagliaroli, T. M., Krauss, R. H., Day, S. W., Reubush, D. E., McClinton, C. R., Reubush, D. E.

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