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- Effect of Reduction in Thickness From 6 to 2 Percent and Removal of the Pointed Tips on the Subsonic Static Longitudinal Stability Characteristics of a 60-Degree Triangular Wing in Combination With a Fuselage
- A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body
- Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule
- A Wind-Tunnel Investigation of the Low-Amplitude Damping in Yaw and Directional Stability of a Fuselage-Tail Configuration at Mach Numbers Up to 1.10