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title: national advisory committee for aeronautics -- report

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    Wind-tunnel investigation of spoiler, deflector, and slot lateral-control devices on wings with full-span split and slotted flaps

    Wenzinger, C.J. / Rogallo, F.M. | Engineering Index Backfile | 1941
    Results of investigation made in NACA 7 by 10-ft wind tunnel; static rolling and yawing moments were determined for all devices tested, and ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Pressure distribution over airfoil section with flap and tab

    Wenzinger, C.J. | Engineering Index Backfile | 1936
    Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United states Advisory Committee for Aeronautics)

    Pressure distribution over rectangular airfoil with partial-span split flap

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1936
    ° and covered range of angles of attack from zero lift to maximum lift for each flap deflection; deflecting partial-span split flap affected ...
    Publisher: National Advisory Committee for Aeronautics

    Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap

    Wenzinger, C.J. / Delano, J.B. | Engineering Index Backfile | 1938
    Data presented in form of pressure distribution diagrams and graphs of calculated section coefficients for airfoil and flap combinations ...
    Publisher: National Advisory Committee for Aeronautics

      Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap

      Wenzinger, C.J. / Delano, J.B. | Engineering Index Backfile | 1938
      Data presented in form of pressure distribution diagrams and graphs of calculated section coefficients for airfoil and flap combinations ...
      Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps

    Wenzinger, C.J. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

      Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps

      Wenzinger, C.J. | Engineering Index Backfile | 1937
      With split flaps of equal length both wings had same CLmax; if 30% of flap outer span were removed for installation of ailerons, reduction ...
      Publisher: National Advisory Committee for Aeronautics

      Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps

      Wenzinger, C.J. | Engineering Index Backfile | 1937
      Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel investigation of aerodynamic balancing of upper-surface ailerons and split flaps

    Wenzinger, C.J. | Engineering Index Backfile | 1935
    Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel investigation of N.A.C.A. 23012, 23021, and 23030 airfoils with various sizes of split flap

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1939
    Final maximum lift coefficients for three airfoils tested with 0.20cw flap were about equal; increase in minimum profile drag coefficient ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Wind tunnel research comparing lateral control devices, particularly at high angles of attack -- XII

    Weick, F.E. / Wenzinger, C.J. | Engineering Index Backfile | 1934
    Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of slotted flaps

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United states Advisory Committee for Aeronautics)

    Characteristics of Clark Y wing model equipped with several forms of low-drag fixed slots

    Weick, F.E. / Wenzinger, C.J. | Engineering Index Backfile | 1932
    Investigation to develop low-drag fixed slot for airplane wing which would avoid complications and maintenance difficulties of present ...
    Publisher: National Advisory Committee for Aeronautics

    Aerodynamic characteristics of slotted clark Y wing as affected by auxiliary airfoil position

    Wenzinger, C.J. / Shortal, J.A. | Engineering Index Backfile | 1931
    Aerodynamic force tests conducted in vertical wind tunnel; increase of 41.5 per cent in max. lift; angle of attack for max. lift increased ...
    Publisher: National Advisory Committee for Aeronautics

    Preliminary wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of venetian-blind flaps

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1940
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Wind-tunnel investigation of N.A.C.A. 23012 airfoil with slotted flap and three types of auxiliary flap

    Wenzinger, C.J. / Gauvain, W.E. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United states Advisory Committee for Aeronautics)

    Wind-tunnel tests of clark Y wing having split flaps with gaps

    Wenzinger, C.J. | Engineering Index Backfile | 1938
    Lift, drag, and pitching moments were measured for wing with three different sizes of flap; it was found that any gap between flap and wing ...
    Publisher: National Advisory Committee for Aeronautics

      Wind-tunnel tests of clark Y wing having split flaps with gaps

      Wenzinger, C.J. | Engineering Index Backfile | 1938
      Lift, drag, and pitching moments were measured for wing with three different sizes of flap; it was found that any gap between flap and wing ...
      Publisher: National Advisory Committee for Aeronautics

    Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing

    Wenzinger, C.J. | Engineering Index Backfile | 1933
    Publisher: National Advisory Committee for Aeronautics

    Wind tunnel pressure distribution tests on an airfoil with trailing edge flap

    Wenzinger, C.J. / Loeser, Jr., O. | Engineering Index Backfile | 1929
    Publisher: National Advisory Committee for Aeronautics

    Pressure distribution over clarke Y-H airfoil section with split flap

    Wenzinger, C.J. | Engineering Index Backfile | 1937
    pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap. ...
    Publisher: National Advisory Committee for Aeronautics

      Pressure distribution over clarke Y-H airfoil section with split flap

      Wenzinger, C.J. | Engineering Index Backfile | 1937
      pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap. ...
      Publisher: National Advisory Committee for Aeronautics

    Resume of air-load data on slots and flaps

    Wenzinger, C.J. / Rogallo, F.M. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Effects of full-span and partial-span split flaps on aerodynamic characteristics of tapered wing

    Wenzinger, C.J. | Engineering Index Backfile | 1934
    Aerodynamic force tests made in wind tunnel using highly tapered Clark Y wing equipped with various split flaps; results given for both ...
    Publisher: National Advisory Committee for Aeronautics

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