Showing 1 - 20 results of 313 for search '', query time: 0.13s Refine Results
  1. 1
    Aeroacoustic measurements of wing-flap configuration /
    Published 1997
    Government Document Book
  2. 2
    Proceedings.
    Published 1965
    Conference Proceeding Book
  3. 3
    Effects of runway unevenness on the dynamic response of supersonic transports /
    Published 1964
    Book
  4. 4
    Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing /
    Government Document Book
  5. 5
    Advanced control technology and its potential for future transport aircraft /
    Published 1976
    Government Document Book
  6. 6
    Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /
    Government Document Book
  7. 7
    Two-layer thermal barrier coating for turbine airfoils - furnace and burner rig test results /
    by Stecura, Stephan
    Published 1976
    Government Document Book
  8. 8
    Fuel-saving aircraft.
    Published 1976
    Government Document Book
  9. 9
    Computer method for design of acoustic liners for turbofan engines /
    by Minner, Gene L., Rice, Edward J.
    Published 1976
    Government Document Book
  10. 10
    Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
    by Blair, A. B.
    Published 1976
    Government Document Book
  11. 11
    Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor /
    by Norgren, Carl T., Ingebo, Robert D.
    Published 1976
    Government Document Book
  12. 12
    Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation /
    Published 1976
    Government Document Book
  13. 13
    Aerodynamic performance of 0.4066-scale model of JT8D refan stage /
    Government Document Book
  14. 14
    Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /
    Government Document Book
  15. 15
    Effect of flame stabilizer design on performance and exhaust pollutants of a two-row 72-module swirl-can combustor /
    by Biaglow, James A.
    Published 1976
    Government Document Book
  16. 16
    Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 /
    Government Document Book
  17. 17
    Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle /
    Government Document Book
  18. 18
    Small, low-cost, expendable turbojet engine : I - design, fabrication, and preliminary testing /
    Government Document Book
  19. 19
    Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged /
    Government Document Book
  20. 20
    Small, low-cost, expendable turbojet engine : II - performance characteristics /
    by Dengler, Robert P.
    Published 1976
    Government Document Book
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