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- Investigation of the Boundary Layer About a Symmetrical Airfoil in a Wind Tunnel of Low Turbulence
- Preliminary Investigation in the NACA Low-Turbulence Tunnel of Low-Drag Airfoil Sections Suitable for Admitting Air at the Leading Edge
- Determination of general relations for the behavior of turbulent boundary layers
- Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-Dimensional Low-Turbulence Pressure Tunnel
- Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company
- Summary of Airfoil Data
- The Langley Two-Dimensional Low-Turbulence Pressure Tunnel
- Low-speed tests of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers
- Note on similarity conditions for flows with heat transfer
- Present status of research on boundary-layer control