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- Calibration of Three Temperature Probes and a Pressure Probe at High Speeds
- Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
- Effect of Compressibility on the Pressure and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-Chord Flap
- Calibrations of Service Pitot Tubes in the Langley 24-Inch High-Speed Tunnel
- Aerodynamics characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8