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  1. 1
    Measurements of supersonic wing tip vortices 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO /

    Measurements of supersonic wing tip vortices 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO /

    Published 1994
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  2. 2
    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges

    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges by Chu, Julio

    Published 1996
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  3. 3
    Distributed system response characteristics in random pressure fields /

    Distributed system response characteristics in random pressure fields / by Barnoski, R. L.

    Published 1970
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  4. 4
    Mir cooperative solar array flight performance data and computational analysis /

    Mir cooperative solar array flight performance data and computational analysis / by Kerslake, Thomas W., Hoffman, David J.

    Published 1997
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  5. 5
    Bidirectional brush seals : post-test analysis /

    Bidirectional brush seals : post-test analysis / by Hendricks, Robert C.

    Published 1997
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  6. 6
    Simulation of turbine tone noise generation using a turbomachinery aerodynamics solver

    Simulation of turbine tone noise generation using a turbomachinery aerodynamics solver by Van Zante, Dale

    Published 2010
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  7. 7
    Approximate pressure distribution in an accelerating launch-vehicle fuel tank

    Approximate pressure distribution in an accelerating launch-vehicle fuel tank by Nemeth, Michael P.

    Published 2010
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  8. 8
    Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /

    Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing / by Laflin, Brenda E. Gile, Applin, Zachary T., Jones, Kenneth M.

    Published 1997
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  9. 9
    A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet /

    A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet / by Moses, Robert W., Pendleton, Ed

    Published 1996
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  10. 10
    Experimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20° /

    Experimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20° / by Stallings, Robert L., Tudor, Dorothy H.

    Published 1969
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  11. 11
    Wind tunnel measured effects on a twin-engine short-haul transport caused by simulated ice accretions : data report /

    Wind tunnel measured effects on a twin-engine short-haul transport caused by simulated ice accretions : data report / by Reehorst, Andrew L.

    Published 1997
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  12. 12
    Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system

    Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system by DeBonis, James R.

    Published 2001
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  13. 13
    Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a crosswind

    Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a crosswind

    Published 1985
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  14. 14
    Experimental effects of wing location on wing-body pressures at supersonic speeds /

    Experimental effects of wing location on wing-body pressures at supersonic speeds / by Allen, Jerry M., Watson, Carolyn B.

    Published 1993
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  15. 15
    Calculation of multistage turbomachinery using steady characteristic boundary conditions

    Calculation of multistage turbomachinery using steady characteristic boundary conditions by Chima, Rodrick V.

    Published 1998
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  16. 16
    Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

    Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters by Bare, E. Ann

    Published 1989
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  17. 17
    NPAC--nozzle performance analysis code

    NPAC--nozzle performance analysis code by Barnhart, Paul J.

    Published 1997
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  18. 18
    Structural analysis and optimization of a composite fan blade for future aircraft engine

    Structural analysis and optimization of a composite fan blade for future aircraft engine by Coroneos, Rula M.

    Published 2012
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  19. 19
    DBD plasma actuators for flow control in air vehicles and jet engines simulation of flight conditions in test chambers by density matching /

    DBD plasma actuators for flow control in air vehicles and jet engines simulation of flight conditions in test chambers by density matching / by Ashpis, D. E. (David E.)

    Published 2011
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  20. 20
    The fast scattering code (FSC) validation studies and program guidelines /

    The fast scattering code (FSC) validation studies and program guidelines / by Tinetti, Ana Fiorella, 1962-

    Published 2011
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