Tests of the NACA 0010-1.50 40/1.051 Airfoil Section at High Subsonic Mach Numbers, report, September 4, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59614/m1/1/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, digital.library.unt.edu; .