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- An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback: Estimated Downwash Angles Derived From Pressure Measurements on the Tail at Mach Numbers of 1.40 and 1.59
- Tables for the computation of wave drag of arrow wings of arbitrary airfoil section
- Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section
- The proper combination of lift loadings for least drag on a supersonic wing
- Span loadings due to wing twist at transonic and supersonic speeds
- The use of pure twist for drag reduction on arrow wings with subsonic leading edges
- A tabulation of wind-tunnel pressure data at Mach numbers of 1.61 and 2.01 of five swept wings of the same plan form but different surface shapes