High-Speed Wind-Tunnel Tests of a 1/14-Scale Model of a Four-Engine Cargo Airplane
Effect of Lateral Shift of Center of Gravity on Rudder Deflection Required for Trim
Wind-tunnel investigation of a 1/20-scale powered model of a four-engine transport airplane
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
Estimation of stick-fixed neutral points of airplanes
Comparison of fixed-stabilizer, adjustable- stabilizer and all-movable horizontal tails
Flight Tests of an Airplane Model with 42 Degree Swept-back Wing in the Langley Free-flight Tunnel
Flight Investigation of Some Factors Affecting the Critical Tail Loads on Large Airplanes