Showing 1 - 20 results of 174 for search '', query time: 0.14s Refine Results
  1. 1
    Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers /

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    Government Document Book
  2. 2
    Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings /

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    Government Document Book
  3. 3
    The induction factor used for computing the rolling moment due to the ailerons /

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    Government Document Book
  4. 4
    Numerical study of transonic flow over oscillating airfoils using the full potential equation /
    by Isogai, Koji
    Published 1978

    Government Document Book
  5. 5
    Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models
    by Peterson, John B
    Published 1988

    Government Document Book
  6. 6
    Two blowing concepts for roll and lateral control of aircraft
    Published 1986

    Government Document Book
  7. 7
    Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models
    by Peterson, John B
    Published 1991

    Government Document Book
  8. 8
    Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control /
    by Blair, A. B
    Published 1978

    Government Document Book
  9. 9
    Design considerations of manipulator and feel system characteristics in roll tracking /
    by Johnston, Donald E
    Published 1988

    Government Document Book
  10. 10
    Tests on an airfoil with two slots suitable for an aircraft of high performance : lift, drag, rolling and yawing moment measurements /
    by Page, F. Handley
    Published 1926

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  11. 11
    Determination of the air forces and moments produced by the ailerons of an airplane /
    by Wieselsberger, C
    Published 1928

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    Government Document Book
  12. 12
    Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds /
    by Margolis, Kenneth
    Published 1950

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    Government Document Book
  13. 13
    Pressure distribution and damping in steady roll at supersonic Mach numbers of flat swept-back wings with subsonic edges /
    by Walker, Harold J
    Published 1950

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    Government Document Book
  14. 14
    Determination of the rate of roll of pilotless aircraft research models by means of polarized radio waves /
    by Harris, Orville R
    Published 1950

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    Government Document Book
  15. 15
    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter /
    by Reeder, John P
    Published 1952

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    Government Document Book
  16. 16
    The Effect of wing bending deflection on the rolling moment due to sideslip /
    by Lovell, Powell M
    Published 1948

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    Government Document Book
  17. 17
    Damping in pitch and roll of triangular wings at supersonic speeds /
    by Brown, Clinton E
    Published 1948

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    Government Document Book
  18. 18
    Analysis of the effects of wing interference on the tail contributions to the rolling derivatives /
    by Michael, William H
    Published 1951

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    Government Document Book
  19. 19
    Damping in roll of cruciform and some related delta wings at supersonic speeds /

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    Government Document Book
  20. 20
    Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds /
    by Martin, John C
    Published 1951

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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