A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2022; you can also visit the original URL.
The file type is application/pdf.
Emma Landrum. "A Study At A Mach Number Of 2.01 Of The Shock Boundary-Layer Interaction Resulting From The Deflection Of A Wedge Mounted On A Bypass Plate." (1961)