Showing 1 - 20 results of 48 for search '', query time: 0.06s Refine Results
  1. 1

    Flutter of control surface tabs / by Naylor, G. A.

    Published 1951
    Book
  2. 2
  3. 3
  4. 4

    Estimation of control forces of spring-tab ailerons from wind-tunnel data / by Deters, Owen J.

    Published 1947
    Government Document Book
  5. 5

    Wind-tunnel investigation of ailerons on a low-drag airfoil. : 3 - The effect of tabs / by Holtzclaw, Ralph W.

    Published 1944
    Government Document Book
  6. 6

    A criterion for the prevention of spring-tab flutter / by Collar, A. R.

    Published 1952
    Book
  7. 7
  8. 8
  9. 9

    The use of geared spring tabs for elevator control / by Phillips Wiliam H.

    Published 1945
    Government Document Book
  10. 10
  11. 11
  12. 12

    Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight / by Kleckner, Harold F.

    Published 1945
    Government Document Book
  13. 13

    Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high Mach numbers / by Kleckner, Harold F.

    Published 1945
    Government Document Book
  14. 14

    Application of spring tabs to elevator controls / by Phillips, William H.

    Published 1944
    Government Document Book
  15. 15

    Calculation of stick forces for an elevator with a spring tab / by Greenberg, Harry

    Published 1944
    Government Document Book
  16. 16

    Effect of spring and gravity moments in the control system on the longitudinal stability of the Brewster XSBA-1 airplane / by Phillips, William H.

    Published 1942
    Government Document Book
  17. 17

    Flight tests of the lateral control characteristics of an F6F-3 airplane equipped with spring-tab ailerons / by Williams, Walter C.

    Published 1945
    Government Document Book
  18. 18

    Tests of a 0.1475c aileron with a tab on low-drag section for Curtiss XP-60 airplane in the low-turbulence tunnel / by Von Doenhoff, Albert E.

    Published 1941
    Government Document Book
  19. 19
  20. 20

    Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons / by Imlay, Frederick H.

    Published 1944
    Government Document Book
Search Tools: RSS Feed Save Search