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  1. 1
    Wind tunnel measurements in the wakes of structures

    Wind tunnel measurements in the wakes of structures by Woo, H. G. C.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  2. 2
    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°

    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° by Mulcay, William

    Washington, D.C. : [Springfield, Va.] :; Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980
    Format: Government Document Book


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  3. 3
    Performance testing of a main rotor system for a utility helicopter at 1/4 scale

    Performance testing of a main rotor system for a utility helicopter at 1/4 scale by Berry, John D.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1982
    Format: Government Document Book


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  4. 4
    The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models

    The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models by Scott, William A. (William Allen), 1958-

    Lawrence, Kan. : Flight Research Laboratory, University of Kansas, Center for Research Inc., 1984
    Format: Government Document Book


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  5. 5
    Applications and requirements for real-time simulators in ground-test facilities

    Applications and requirements for real-time simulators in ground-test facilities by Arpasi, Dale J.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  6. 6
    Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests

    Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests by Freeman, Delma C.

    [Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [National Aeronautics and Space Administration, Scientific and Technical Information Branch] ; [For sale by the National Technical Information Service],; National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
    Format: Government Document Book


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  7. 7
    Wind-tunnel test of an articulated helicopter rotor model with several tip shapes

    Wind-tunnel test of an articulated helicopter rotor model with several tip shapes by Berry, John D.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ; [Fo r sale by the National Technical Information Service], 1980
    Format: Government Document Book


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  8. 8
    A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

    A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel by Lawing, Pierce L.

    Washington, D.C. : [Springfield, Va.] :; Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service],; National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
    Format: Government Document Book


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  9. 9
    Closed-test-section wind tunnel blockage corrections for road vehicles.

    Closed-test-section wind tunnel blockage corrections for road vehicles.

    Warrendale, Pa. : Society of Automotive Engineers, 1996
    Format: Conference Proceeding Book


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  10. 10
    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊: I - low-wing model C

    Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊: I - low-wing model C by Mulcay, William

    Washington, D.C. : [Springfield, Va.] :; Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980
    Format: Government Document Book


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  11. 11
    Applications and requirements for real-time simulators in ground-test facilities

    Applications and requirements for real-time simulators in ground-test facilities by Arpasi, Dale J.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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