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  1. 1
    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., Spencer, Bernard, 1932-

    Published 1980
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  2. 2
    Wind tunnel measurements in the wakes of structures /

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

    Published 1977
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  3. 3
    Wind-tunnel investigation of the horizontal motion of a wing near the ground /

    Wind-tunnel investigation of the horizontal motion of a wing near the ground / by Serebrisky, Y. M.

    Published 1946
    Government Document Book
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  4. 4
    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.

    Published 1980
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  5. 5
    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

    Published 1980
    Government Document Microfilm Book
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  6. 6
    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.

    Published 1980
    Government Document Microfilm Book
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  7. 7
    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

    Published 1980
    Government Document Book
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  8. 8
    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.

    Published 1980
    Government Document Microfilm Book
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  9. 9
    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.

    Published 1982
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  10. 10
    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, Chu, Julio

    Published 1980
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  11. 11
    Environmental impact statement amendment no. 1 to the 1977 institutional environmental impact statement for the Ames Research Center : modification of the 40- by 80-foot subsonic wind tunnel.

    Environmental impact statement amendment no. 1 to the 1977 institutional environmental impact statement for the Ames Research Center : modification of the 40- by 80-foot subsonic w...

    Published 1977
    Government Document Microfilm Book
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  12. 12
    Closed-test-section wind tunnel blockage corrections for road vehicles.

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

    Published 1996
    Conference Proceeding Book
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  13. 13
    Advanced hypersonic test facilities /

    Advanced hypersonic test facilities /

    Published 2002
    Book
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