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- Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method
- Theoretical investigation of some discontinuous yaw dampers
- Correlation of flight and analog investigations of roll coupling
- Some recent research on the handling qualities of airplanes
- Spinning and related problems at high angles of attack for high-speed airplanes
- A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver
- Flight and analytical study of roll requirements of a fighter airplane