Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 /

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Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range / by Bursnall, William J.

Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges / by Margolis, Kenneth

Experimental investigation of the low-speed static and yawing stability characteristics of a 45 degree sweptback high-wing configuration with various twin vertical wing fins / by Goodman, Alex

Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations / by Howard, Donald A.

Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds / by Martin, John C.

The response of an aeroplane to the application of ailerons and rudders. by Gandy, R. W.

Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / by Bamber, M. J

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Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane / by Sternfield, Leonard

Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. by Harmon, Sidney M.

Effect of an autopilot sensitive to yawing velocty on the lateral stability of a typical high-speed airplane / by Gates, Ordway B.

Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel / by Bird, J. D.

Calculation of aerodynamic forces on a propeller in pitch or yaw / by Crigler, John L.

Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41 / by Coletti, Donald E.

Helicopter instrument flight and precision maneuvers as affected by changes in damping in roll, pitch, and yaw / by Whitten, James B.

Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory condition... by Queijo, M. J.

Experimental steady-state yawing deriviatives of a 60 degree delta-wing model as affected by changes in vertical position of the wing and in ratio of fuselage diameter to wing span... by Jaquet, Byron M.

Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence / by Eggleston, John M.

A theoretical method of analyzing the effects of yaw-damper dynamics on the stability of an aircraft equipped with a second-order yaw damper / by Schy, Albert A.

A theoretical and experimental investigation of the effects of yaw on pressures, forces, and moments during seaplane landings and planing / by Smiley, Robert F.