Mean velocity and turbulence data at Mach 2.9 for 8, 16 and 20 degree compression corners, a reattaching shear layer, two concavely curved walls, and an adverse pressure gradient.

• Compilation of Turbulence Data for 20 degree Compression Corner at Mach 2.9 (MAE Report 1620, December 1983)
• Compilation of Turbulence Data for a 16 degree Compression Corner at Mach 2.9 (MAE Report 1619, November 1983)
• Compilation of Turbulence Data for an 8 degree Compression Corner at Mach 2.9 (MAE Report 1642, April 1984)
• Compilation of Turbulence Data for a Reattaching Shear Layer at Mach 2.9 (MAE Report 1601, April 1983)
• Compilation of Turbulence Data for Two Concavely Curved Walls at Mach 2.9 (MAE Report 1711, August 1985)
• A Data Compilation for a Supersonic Turbulent Boundary Layer Under Conditions of an Adverse Pressure Gradient (MAE Report 1746, May 1986)