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Laminar-turbulent transition in a mach 8 elliptic cone flow
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Kimmel, R. L., Poggie J., and Schwoerke S. N., "Laminar-Turbulent Transition in a Mach 8 Elliptic Cone Flow," AIAA Journal, Vol. 37, No. 9, September 1999, pp. 1080-1087.
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67650963651
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Pressure and heat transfer distribution on ASD elliptic cone (W3) and ASD sortie (W4) in the CAL 48-inch hypersonic shock tunnel
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December, ASC 94 2649
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Nowlan, D., Burke, A., and Bird, K., "Pressure and Heat Transfer Distribution on ASD Elliptic Cone (W3) and ASD Sortie (W4) in the CAL 48-Inch Hypersonic Shock Tunnel," CAL Report AM-1800-Y-2, December 1963. ASC 94 2649.
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Mechanisms of plasma actuators for hypersonic flow control
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Shang, J. S., Surzhikov, S. T., Kimmel, R., Gaitonde, D., Menart, J., and Hayes, J., "Mechanisms of Plasma Actuators for Hypersonic Flow Control," Progress in Aerospace Sciences, Vol. 41, No. 8, November 2005, pp. 642-668.
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Computational study of shock mitigation and drag reduction by pulsed energy lines
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Kremeyer, K., Sebastian, K., and Shu, C.-W., "Computational Study of Shock Mitigation and Drag Reduction by Pulsed Energy Lines," AIAA Journal, Vol. 44, No. 8, August 2006.
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Control of Edney IV Interaction by Energy Pulse
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Yan, H.1
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AIAA paper 2002-0129, American Institute of Aeronautics and Astronautics, Reno NV, January
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Girgis, I. G., Shneider, M. N., Macheret, S. O., Brown, G. L., and Miles, R. B., "Creation of Steering Moments in Supersonic Flow by Off-Axis Plasma Heat Addition," AIAA paper 2002-0129, American Institute of Aeronautics and Astronautics, Reno NV, January 2002.
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Creation of Steering Moments in Supersonic Flow by Off-Axis Plasma Heat Addition
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Girgis, I.G.1
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AIAA paper 2006-1172, American Institute of Aeronautics and Astronautics, Reno NV, January
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Menart, J., Stanfield, S., Shang, J., Kimmel, R., and Hayes, J., "Study of Plasma Electrode Arrangements for Optimum Lift in a Mach 5 Flow," AIAA paper 2006-1172, American Institute of Aeronautics and Astronautics, Reno NV, January 2006.
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Study of Plasma Electrode Arrangements for Optimum Lift in a Mach 5 Flow
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12
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AIAA paper 2005-164, American Institute of Aeronautics and Astronautics, Reno NV, January
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Updike, G. A., Shang, J. S., and Gaitonde, D. V., "Hypersonic Separated Flow Control Using Magneto-Aerodynamic Interaction," AIAA paper 2005-164, American Institute of Aeronautics and Astronautics, Reno NV, January 2005.
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AIAA paper 2006-710, American Institute of Aeronautics and Astronautics, Reno NV, January
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Kimmel, R. L., Hayes, J. R., Crafton., J. W., Fonov, S. D., Menart, J., and Shang, J., "Surface Discharge for High-Speed Boundary Layer Control," AIAA paper 2006-710, American Institute of Aeronautics and Astronautics, Reno NV, January 2006.
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Surface Discharge for High-Speed Boundary Layer Control
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AIAA paper 2005-561, American Institute of Aeronautics and Astronautics, Reno NV, January
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Poggie J., "Plasma-Based Hypersonic Flow Control," AIAA Paper 2006-3567, American Institute of Aeronautics and Astronautics, San Francisco CA, June 2006.
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Poggie, J.1
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18
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0031186560
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Three-dimensional hypersonic laminar boundary-layer computations for transition experiment design
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July-August
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Kimmel, R., Klein, M., Schwoerke, S., "Three-Dimensional Hypersonic Laminar Boundary-Layer Computations for Transition Experiment Design," AIAA Journal, Vol. 34 No. 4, July-August 1997, pp. 409-415.
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Heat transfer and pressure distributions about sharp and blunt elliptic cones at angles of attack and high mach numbers
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Wright-Patterson AFB, OH, May
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AIAA Paper 2003-329, American Institute of Aeronautics and Astronautics, Reno NV, January
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Shang, J., Kimmel, R., Hayes, J., and Tyler, C., "Performance of a Low-Density Hypersonic Magneto-Aerodynamic Facility," AIAA Paper 2003-329, American Institute of Aeronautics and Astronautics, Reno NV, January 2003.
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Performance of a Low-Density Hypersonic Magneto-Aerodynamic Facility
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22
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85087598124
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AIAA Paper 2003-4165, American Institute of Aeronautics and Astronautics, Reno NV, January
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Menart, J., Shang, J., Kimmel, R., and Hayes, J., "Effects of Magnetic Fields on Plasmas Generated in a Mach 5 Wind Tunnel," AIAA Paper 2003-4165, American Institute of Aeronautics and Astronautics, Reno NV, January 2003.
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Effects of Magnetic Fields on Plasmas Generated in a Mach 5 Wind Tunnel
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AIAA Paper 2004-509, American Institute of Aeronautics and Astronautics, Reno NV, January
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Kimmel, R. L., Hayes, J. R., Menart, J. A., and Shang, J., "Effect of Surface Plasma Discharges on Boundary Layers at Mach 5," AIAA Paper 2004-509, American Institute of Aeronautics and Astronautics, Reno NV, January 2004.
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Effect of Surface Plasma Discharges on Boundary Layers at Mach 5
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AIAA Paper 2004-2661, American Institute of Aeronautics and Astronautics, Reno NV, January
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Kimmel, R., Hayes, J., Menart, J., and Shang, J., "Effects on Magnetic Fields on Surface Plasma Discharges at Mach 5," AIAA Paper 2004-2661, American Institute of Aeronautics and Astronautics, Reno NV, January 2004.
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Effects on Magnetic Fields on Surface Plasma Discharges at Mach 5
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25
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AIAA Paper 2004-2264, American Institute of Aeronautics and Astronautics, Reno NV, January
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Menart, J., Henderson, S., Shang, J., Kimmel, R., Hayes, J., "DC Plasma Discharge Effects on a Mach 5 Flow Between Small Plate Electrodes," AIAA Paper 2004-2264, American Institute of Aeronautics and Astronautics, Reno NV, January 2004.
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DC Plasma Discharge Effects on a Mach 5 Flow between Small Plate Electrodes
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Hayes, J.5
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26
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67650944952
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Supersonic plasma flow control experiments
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Wright-Patterson Air Force Base, OH, December
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Kimmel, R., Hayes, J., Menart, J., and Shang, J, "Supersonic Plasma Flow Control Experiments," U.S. Air Force Research Lab., TR ARFL-VA-WP-TR-2006-3006, Wright-Patterson Air Force Base, OH, December 2005.
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