Showing 1 - 13 results of 13 for search '', query time: 0.16s Refine Results
  1. 1
    A moving-belt rig for ground simulation in low-speed wind tunnels /
    by Butler, S. F. J.
    Published 1967
    Book
  2. 2
    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 Book
  3. 3
    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
  4. 4
    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 Book
  5. 5
    Wind-tunnel test of an articulated helicopter rotor model with several tip shapes /
    by Berry, John D.
    Published 1980
    Government Document Book
  6. 6
    Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG] /
    by Mulcay, William
    Published 1980
    Government Document Book
  7. 7
    Performance testing of a main rotor system for a utility helicopter at 1/4 scale /
    by Berry, John D.
    Published 1982
    Government Document Book
  8. 8
    The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models /
    Government Document Book
  9. 9
    Applications and requirements for real-time simulators in ground-test facilities /
    by Arpasi, Dale J.
    Published 1986
    Government Document Book
  10. 10
    The measurement of ground effect using a fixed ground board in a wind tunnel /
    by East, L. F.
    Published 1972
    Book
  11. 11
    Advanced hypersonic test facilities /
    Published 2002
    Book
  12. 12
    Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests /
    Get full text
    Government Document eBook
  13. 13
    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
    Get full text
    Government Document eBook
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