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4
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33845588519
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Experimental and computational investigation of cavity flows simulating damage to thermal protection system tiles
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Everhart, J. L., Bey, K. S., Wood, W. A., and Pulsonetti, M. V.: "Experimental and Computational Investigation of Cavity Flows Simulating Damage to Thermal Protection System Tiles," Presented at 21st JANNAF Airbreathing Propulsion Subcommittee, Colorado Springs, CO, Dec. 1-5, 2003.
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21st JANNAF Airbreathing Propulsion Subcommittee
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Everhart, J.L.1
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Pulsonetti, M.V.4
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5
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34250894428
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AIAA 2006-0185
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Pressure Gradient Effects on Hypersonic Cavity Flow Heating
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Prabhu, R.K.5
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6
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84888819535
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Boundary layer/streamline surface catalytic heating predictions on space shuttle orbiter
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Marichalar, J. J., Rochelle, W. C., Kirk, B. S., and Campbell, C. H., "Boundary Layer/Streamline Surface Catalytic Heating Predictions on Space Shuttle Orbiter," Journal of Spacecraft and Rockets, (to be published).
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7
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AIAA 2004-2635
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Alter, S.J.1
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9
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Reuther, J.J.1
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10
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-
Catalytic heating of Reinforced Carbon-Carbon (RCC) repair materials
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Grinstead, J. H., Ellerby, D. T., Prabhu, D., McDaniel, R. D., Squire, T. H., Bahrami, P., and Campbell, C. H., "Catalytic Heating of Reinforced Carbon-Carbon (RCC) Repair Materials," NASA/TM 2006-213480.
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11
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Overview of Boundary Layer Transition Research in Support of Return to Flight
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Berry, S.A.1
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12
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AIAA 2006-2919
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Horvath, T. J., Berry, S. A., Merski, N. R., Berger, K. T., Buck, G. M., Liechty, D. S., and Schneider, S. P., "Shuttle Damage / Repair From the Perspective of Hypersonic Boundary Layer Transition - Experimental Results," AIAA 2006-2919, 2006.
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Greene, F., Hamilton, H., and Weilmuenster, K. J., "Development of a Boundary Layer Properties Interpolation Tool in Support of Orbiter Return-To-Flight,"AIAA 2006-2920, 2006.
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AIAA-2006-2922, June
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Berry, S. A., Horvath, T. J., Cassady, A., Kirk, B. S., Wang, K.C., and Hyatt, A. J., "Boundary Layer Transition Results From STS-114," AIAA-2006-2922, June 2006.
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Berry, S.A.1
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Hyatt, A.J.6
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