Performance Potential and Research Needs of a Hypersonic, Airbreathing, Lifting Missile Concept von Hunt, J. L, Lawing, P. L, Marcum, D. C, Cubbage, J. M

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Transonic unsteady pressure measurements on a supercritical airfoil at high Reynolds numbers von Hess, Robert W, Seidel, David A, Igoe, William B, Lawing, Pierce L

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The construction of airfoil pressure models by the plate method: Achievements, current research, technology development and potential applications von Lawing, P. L.

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Configuration heating for a hypersonic research airplane concept having a 70 deg swept double-delta wing von Lawing, P. L.

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Analysis of various descent trajectories for a hypersonic-cruise, cold-wall research airplane von Lawing, P. L.

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Experimental study of stagnation enthalpy in the Langley hotshot tunnel von Lawing, P. L.

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Inlet Boundary-Layer Shapes on Four Aircraft Forebodies at Mach 6 von Lawing, Pierce L, Johnson, Charles B

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Mach 6 flowfield survey at the engine inlet of a research airplane von Johnson, Charles B, Lawing, Pierce L

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Aerodynamic heat transfer to a hypersonic research aircraft model /X-24C/ at Mach 6 von Lawing, Pierce L, Hunt, James L

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Measurements in the flow field of a cylinder with a laser transit anemometer and a drag rake in the Langley 0.3 m transonic cryogenic tunnel von Honaker, W. C., Lawing, P. L.

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Cooling system for high speed aircraft von Lawing, P. L., Pagel, L. L.

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Support interference of wind tunnel models: A selective annotated bibliography von Tuttle, M. H., Lawing, P. L.

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Flow rate/pressure drop data gathered from testing a sample of the Space Shuttle Strain Isolation Pad (SIP): Effects of ambient pressure combined with tension and compression condi... von Springfield, R. D., Lawing, P. L.

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Orbiter thermal pressure drop characteristics for shuttle orbiter thermal protection system components: High density tile, low density tile, densified low density tile, and strain... von Lawing, P. L., Nystrom, D. M.

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Cryogenic wind tunnels for high Reynolds number testing von Lawing, P. L., Kilgore, R. A., Mcguire, P. D.

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Description of the insulation system for the Langley 0.3-Meter Transonic Cryogenic Tunnel von Lawing, P. L., Dress, D. A., Kilgore, R. A.

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A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3 meter transonic cryogenic tunnel von Lawing, P. L., Adcock, J. B., Ladson, C. L.

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Hypersonic Airbreathing Missile von Hunt, J. L., Lawing, P. L., Marcum, D. C., Jr

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Merging paleobiology with conservation biology to guide the future of terrestrial ecosystems von Barnosky, Anthony D., Hadly, Elizabeth A., Gonzalez, Patrick, Head, Jason, Polly, P. David, Lawing, A. Michelle, Eronen, Jussi T., Ackerly, David D., Alex, Ken, Biber, Eric, Blois, Jessica, Brashares, Justin, Ceballos, Gerardo, Davis, Edward, Dietl, Gregory P., Dirzo, Rodolfo, Doremus, Holly, Fortelius, Mikael, Greene, Harry W., Hellmann, Jessica, Hickler, Thomas, Jackson, Stephen T., Kemp, Melissa, Koch, Paul L., Kremen, Claire, Lindsey, Emily L., Looy, Cindy, Marshall, Charles R., Mendenhall, Chase, Mulch, Andreas, Mychajliw, Alexis M., Nowak, Carsten, Ramakrishnan, Uma, Schnitzler, Jan, Shrestha, Kashish Das, Solari, Katherine, Stegner, Lynn, Stegner, M. Allison, Stenseth, Nils Chr, Wake, Marvalee H., Zhang, Zhibin

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Description and initial calibration of the langley hotshot tunnel with some real-gas charts for nitrogen von Harrison, E. F., Lawing, P. L., Smith, F. M.

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