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- A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36©�
- Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
- A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
- Heat transfer to bodies at angles of attack