The use of geared spring tabs for elevator control
Explore the source record for details and available documents.
AIRPLANES, GIANT↗
SEARCH · Engineering Papers
Results for “TaB”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Wind tunnel investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil
Explore the source record for details and available documents.
TABS - DEFLECTION↗
Estimation of control forces of spring-tab ailerons from wind-tunnel data
Explore the source record for details and available documents.
AILERON CONTROLS↗
Flight Tests of a Rudder with a Spring Tab on an F6F-3 Airplane (Buaer No.04776)
Explore the source record for details and available documents.
AIRPLANES-GRUMMAN F6F-3 FLIGHT TESTS (AMER )↗
Calculation of stick forces for an elevator with a spring tab
Explore the source record for details and available documents.
CONTROL STICKS - FORCES↗
Wind-Tunnel Tests of Hinge-Moment Characteristics of Spring-Tab Ailerons
No abstract available
TABS, AILERON↗
Flight Tests of an All-movable Horizontal Tail with Geared Unbalancing Tabs on the Curtiss XP-42 Airplane
Explore the source record for details and available documents.
AIRPLANES - CURTISS P-36A (AMER)↗
Investigation of an Approximately 0.178-chord-thick NACA 6-series-type Airfoil Section Equipped with Sealed Internally Balanced 0.20-chord Ailerons and with a 0.05-chord Tab
Explore the source record for details and available documents.
TABS, AILERON↗
Flight investigation of a combined geared unbalancing-tab and servotab control system as used with an all-movable horizontal tail
Explore the source record for details and available documents.
STABILITY & CONTROL, LONGITUDINAL - CURTISS P-42↗
Wind-tunnel investigation of trimming tabs on a thickened and beveled aileron on a tapered low-drag wing
Explore the source record for details and available documents.
LATERAL CONTROL DEVICES LMAL↗
Calculation of tab characteristics for flight conditions from wind-tunnel data
Explore the source record for details and available documents.
ELEVATORS - DEFLECTION↗
Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight
Explore the source record for details and available documents.
CONTROL STICKS - FORCES↗
Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing I : aileron with fixed inset tabs
Explore the source record for details and available documents.
TABS, AILERON↗
Tests of a 0.1475c aileron with a tab on low-drag section for Curtiss XP-60 airplane in the low-turbulence tunnel
Explore the source record for details and available documents.
AIRFOILS - NACA 66,2-118 - CHARACTERISTICS LOW-DRA↗
Vacuum thermionic work functions and thermal stability of TaB sub 2, ZrC, Mo sub 2 C, MoSi sub 2, TaSi sub 2, and WSi sub 2.
Vacuum thermionic work function and thermal stability measurements on crystal surfaces, discussing results on carbides, diborides and disilicades
THERMIONIC EMISSION↗
Electron and ion emission from surfaces originally of TaB sub 2, ZrC, Mo sub 2 C, MoSi sub 2, TaSi sub 2, and WSi sub 2 in cesium vapor.
Surface electron and ion emission from refractory metal compounds in cesium vapor, showing electron emission S curves and surface ionization critical temperature envelopes
Wilson, R. G.↗
The influence of composition and thermomechanical condition on mechanical properties of TaC and TaB strengthened chromium
Explore the source record for details and available documents.
Filippi, A. M.↗
Methods for measuring plating thicknesses on TAB lead frames
Plating three layer tape lead frames, used for tape automated bonding, offers a challenge to the electroplater because of nonuniform topography. Each lead frame contains large (typically .05 x. .05 inch) flat test pads located around the perimeter of the frame. These test pads are electrically connected to the bondable lead frame fingers which extend into an area in the center of the frame called the feature hole. The feature hole exposes these fingers to plating on all sides, while the test pads are exposed on only one side. In addition, the fingers are small in cross section (typically .003 x .0015 inches). Recent thickness measurements indicate that plating around the lead frame fingers is nearly twice as thick as that on test pad areas. Procedures and equipment were developed for measuring the thickness of the deposited material. Discussion was centered on the data obtained using the various measurement techniques and equipment.
Hagen, M. P.↗