Search Results

Wind-tunnel investigation of effects of various aerodynamic balance shapes and sweepback on control-surface characteristics of semispan tail surfaces with NACA 0009, 0015, 66-009,... by Harper, John J.

Theoretical characteristics of two-dimensional supersonic control surfaces / by Morrissette, Robert R.

Lift on a bent, flat plate / by Keune, F.

Theoretical study of some methods for increasing the smoothness of flight through rough air / by Phillips, William H.

Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. : Mach lines behnid flap leading and trailing edges / by Kainer, Julian H.

Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds / by DeYoung, John

Search for the full-text version of this title in HathiTrust

Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data / by Sivells, James C.

Search for the full-text version of this title in HathiTrust

Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of apsect ratio 1.59 equipped with various 25-percent-chord plain flaps / by Johnson, Harold S.

Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / by Turner, M. J.

Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations / by Piland, Robert O.

Search for the full-text version of this title in HathiTrust

Influence of airfoil trailing-edge angle and trailing-edge thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers / by Hemenover, Albert D.

Use of two-dimensional data in estimating loads on a 45 degree sweptback wing with slats and partial-span flaps / by Hunton, Lynn W.

Investigation of a slat in several different positions on an NACA 64A010 airfoil for a wide range of subsonic Mach numbers / by Axelson, John A.

Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes / by Weick, Fred E.

Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight / by Kuhn, Richard E.

Some effects of propeller operation and location on ability of a wing with plain flaps to deflect propeller slipstreams downward for vertical take-off / by Draper, John W.

Hovering flight tests of a four-engine-transport vertical take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream / by Tosti, Louis P.

Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane / by Dannenberg, Robert E.

A limited flight investigation of the effect of three vortex-generator configurations on the effectiveness of a plain flap on an unswept wing / by Morris, Garland J.

Effect of high-lift devices on the low-speed static lateral and yawing stability characteristics of an untapered 45 degree sweptback wing / by Lichtenstein, Jacob H.