Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing, both having 45 degrees of sweepback Page: 30 of 124
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NACA RM A51D27
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Figure 6.- The measured variation of drag coefficient with Mach number of the
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R, 2,000, 000.Measured drag data
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Johnson, Ben H., Jr. & Shibata, Harry H. Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing, both having 45 degrees of sweepback, report, July 12, 1951; (https://digital.library.unt.edu/ark:/67531/metadc58856/m1/30/: accessed April 19, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.