Lateral-directional aerodynamic characteristics of light, twin-engine, propeller-driven airplanes / by Wolowicz, Chester H., Yancey, Roxanah B.

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

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The estimation of the rate of change of yawing moment with sideslip / by Imlay, Frederick H.

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Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight / by Troller, T., Rokus, F.

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

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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. by Bamber, M. J., House, R. O.

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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. by Bamber, M. J., House, R. O.

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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. by Recant, Isidore G., Wallace, Arthur R.

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

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Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight / by Rokus, Frank G.

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The theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance / by Imlay, Frederick H.

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Wind-tunnel investigation of the effect of vertical position of the wing on the side flow in the region of the vertical tail / by Recant, Isidore G., Wallace, Arthur R.

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Comparison of vee-type and conventional tail surfaces in combination with fuselage and wing in the variable-density tunnel / by Greenberg, Harry

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Wind tunnel tests of five strut sections in yaw / by Warner, Edward Pearson, 1894-1958

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

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The effect of slots and flaps on lateral control of a low-wing monoplane as determined in flight / by Soule, Hartley A. 1904-1988, Wetmore, J. W.

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Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance / by Bamber, M. J., Zimmerman, C. H.

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Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) / by Heald, R. H.

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Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow / by Queijo, M. J.

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