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  1. 1
    Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine : II - effect of air ejection on turbine performance /
    by Haas, Jeffrey E.
    Published 1977
    Government Document Book
  2. 2
    Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : II-performance with coolant flow ejection at temperature ratios up to 2 /
    by Haas, Jeffrey E.
    Published 1977
    Government Document Book
  3. 3
    Effect of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration /
    by Yip, Long P.
    Published 1977
    Government Document Book
  4. 4
    Parametric study of ascent performance of a vertically launched hydrogen-fueled single-stage reusable transport /
    by Rehder, John J.
    Published 1978
    Government Document Book
  5. 5
    Description of path-in-the-sky contact analog piloting display /
    by Knox, Charles E.
    Published 1977
    Government Document Book
  6. 6
    Use of sensitivity analysis to predict performance as a function of different displays /
    by Mout, Michael L.
    Published 1977
    Government Document Book
  7. 7
    Measurements of the tonal component of cavity noise and comparison with theory /
    by Block, Patricia J W.
    Published 1977
    Government Document Book
  8. 8
    Light airplane crash test at impact velocities of 13 and 27 m/sec /
    by Alfaro-Bou, Emilio
    Published 1977
    Government Document Book
  9. 9
    F 100 multivariable control synthesis program, evaluation of a multivariable control using a real-time engine simulation /
    Published 1978
    Government Document Book
  10. 10
    Altitude test of several afterburner configurations on a turbofan engine with a hydrogen heater to simulate an elevated turbine discharge temperature : Roy L. Johnsen and Richard R. Cullom.
    by Johnsen, Roy L.
    Published 1977
    Government Document Book
  11. 11
    Predication of ground effects on aircraft noise /
    by Pao, S. Paul
    Published 1978
    Government Document Book
  12. 12
    Phugoid characteristics of YF-12 airplane with variable-geometry inlets obtained in flight tests at a Mach number of 2.9 /
    by Powers, Bruce G.
    Published 1977
    Government Document Book
  13. 13
    Effects of land approach methods and separation intervals on single runway landing capacity /
    by Hastings, Earl C.
    Published 1977
    Government Document Book
  14. 14
    Eigenvalue/eigenvector assignment using output feedback /
    by Srinathkumar, S.
    Published 1978
    Government Document Book
  15. 15
    Effects of winglets on first-generation jet transport wing : IV - Stability characteristics for a full-span at Mach 0.30 /
    by Meyer, Robert R.
    Published 1978
    Government Document Book
  16. 16
    Analytical study of ride smoothing benefits of control system configurations optimized for pilot handling qualities /
    by Powers, Bruce G.
    Published 1978
    Government Document Book
  17. 17
    Comparison of capabilities and costs of dedicated airplane and spacecraft missions for remote water monitoring of U.S. coastal zones /
    by Darnell, Wayne L.
    Published 1977
    Government Document Book
  18. 18
    Aerodynamic characteristics of airplanes at high angles of attack /
    by Chambers, Joseph R.
    Published 1977
    Government Document Book
  19. 19
    A new blade element method for calculating the performance of high and intermediate solidity axial flow fans /
    by Borst, Henry V.
    Published 1978
    Government Document Book
  20. 20
    Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing /
    by Perry, Boyd
    Published 1978
    Government Document Book
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