Browse TRAIL Inventories

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


Published Year

Author