Investigation of small surface protuberances upstream of turbulent boundary layer separation produced by a skewed shock wave at Mach 3 /

"Interim report for period January 1976-February 1976."

Chemical non-equilibrium shock flow,

"Work performed for the Ballistic Systems Divisions, USAF, under Contract no. AF04(647)-617."

Shock tube test time limitation due to turbulent wall boundary layer.

At head of title: SSD-TDR-63-78. Report no. TDR-169 (3230-12)TR-3.