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- The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel With and Without Nacelles at Mach Numbers From 0.30 to 0.86
- Force Tests of Three Thin Wings of Moderately Low Aspect Ratio at High Subsonic Mach Numbers
- Fuselage Pressures Measured on the Bell X-1 Research Airplane in Transonic Flight
- Flight-determined pressure distributions over a section of the 35 degree swept wing of the Douglas D-558-II research airplane at Mach numbers up to 2.0
- Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds