The induction factor used for computing the rolling moment due to the ailerons / by Munk, Max M. (Max Michael), 1890-

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Theoretical span loading and moments of tapered wings produced by aileron deflection / by Pearson, Henry A. (Henry Adolph), 1906-

Pressure distribution and damping in steady roll at supersonic Mach numbers of flat swept-back wings with subsonic edges / by Walker, Harold J.

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

The Effect of slots and flaps on lateral control of a low-wing monoplane as determined in flight / by Soule, Hartley A. (Hartley Akin), 1904-1988

Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / by Shortal, Joseph Adams, 1908-

Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings / by Weick, Fred E.

Effect of length of Handley Page tip slots on the lateral-stability factor, damping in roll / by Weick, Fred E.

Rolling, yawing, and hinge moments produced by rectangular ailerons / by Heald, R. H.

The Effect of wing tip floating ailerons on the autorotation of a monoplane wing model / by Knight, Montgomery

Low-speed static lateral and rolling stability characteristics of a series of configurations composed of intersecting triangular plan-form surfaces / by Thomas, David F.

Theoretical calculations of the pressures, forces, and moments due to various lateral motions acting on thin isolated vertical tails with supersonic leading and trailing edges / by Margolis, Kenneth

Flight investigation of the roll requirements for transport airplanes in the landing approach / by Holleman, Euclid C., Powers, Bruce G.

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Correlation of two experimental methods of determining the rolling characteristics of unswept wings / by MacLachlan, Robert

Flight tests of retractable ailerons on a highly tapered wing / by Wetmore, J. W. (Joseph W.)

Preliminary study of the damping factor in roll / by Shoemaker, J. M. (James Maurice), Lee, John Glessner, 1898-1988

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Subsonic roll-damping characteristics of a series of wings / by Boyden, Richmond P.

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Comparison of the control-force characteristics of two types of lateral-control system for large airplanes / by Deters, Owen J.

Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degrees, 42 degrees, and 62 degrees sweepback / by Bennett, Charles V.

The effect of wheel alignment on rolling resistance - a literature search and analysis / by Yurko, John

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