Airplanes + Control surfaces
Label
Airplanes + Control surfaces
Name
Airplanes + Control surfaces
Sub focus
Actions
Incoming Resources
- Subject of22
- Flight tests of retractable ailerons on a highly tapered wing, by J.W. Wetmore
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Richard W. Noyes, X
- Analysis of available data on the effects of tabs on control-surface hinge moments, by Stewert M. Crandall and Harry E. Murray
- The elimination of dead center in the controls of airplanes with thick sections, by Thomas Carroll
- Airplanes in horizontal curvilinear flight, by Heinrich Kann
- Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot, by Fred E. Weick and Robert C. Platt
- The reduction of aileron operating force by differential linkage, by Robert T. Jones and Albert I. Nerken
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Carl J. Wenzinger, VII
- Effect of retractable-spoiler location on rolling- and yawing-moment coefficents, J.A. Shortal
- Aerothermal environment in chordwise gaps between split elevons at Mach 6.8, L. Roane Hunt
- Determination of control-surface characteristics from NACA plain-flap and tab data, by Milton B. Ames, Jr., and Richard I. Sears
- The effect on rudder control of slip stream body, and ground interference, by H.I. Hoot and D.L. Bacon
- Wind-tunnel investigation of fuselage stability in yaw with various arrangements of fins, by H. Page Hoggard, Jr
- Downwash of airplane wings, by Max Munk and Gunther Cario
- An instrument for recording the position of airplane control surfaces, by K.M. Ronan
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Carl J. Wenzinger, IX
- Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance, by M.J. Bamber and C.H. Zimmerman
- Pressure-distributioin investigation of an N.A.C.A. 0009 airfoil with an 80-percent-chord plain flap and three tabs, by Milton B. Ames, Jr., and Richard I. Sears
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Thomas A. Harris, XI
- Wind-tunnel tests of three lateral-control devices in combination with a full-span slotted flap on an N.A.C.A. 23012 airfoil, by Carl J. Wenzinger and Millard J. Bamber
- Flight and wind-tunnel tests of an XBM-1 dive bomber, by Philip Donely and Henry A. Pearson
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Joseph A. Shortal, VIII
Outgoing Resources
- Focus1
- Sub focus2