Aerodynamic characteristics at a Mach number of 1.38 of four wings of aspect ratio 4 having quarter-chord sweep angles of 0 degrees, 35 degrees, 45 degrees, and 60 degrees Page: 1 of 43
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AERODYNAMIC CHARACTERISTICS AT A MACHJNUMBER OF 1.38
OF FOUR WINGS OF ASPECT RATIO 4 HAVING QUARTER-
CHORD SWEEP ANGLES OF 00, 350, 450, AND 600
By William B. Kemp, Jr., Kenneth W. Goodson,
and Robert A. Booth
Langley Aeronautical Laboratory
Langley Air Force Base, Va.
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NATIONAL ADVISORY COMMITTEE
October 10, 1950
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Kemp, William B., Jr.; Goodson, Kenneth W. & Booth, Robert A. Aerodynamic characteristics at a Mach number of 1.38 of four wings of aspect ratio 4 having quarter-chord sweep angles of 0 degrees, 35 degrees, 45 degrees, and 60 degrees, report, October 10, 1950; (digital.library.unt.edu/ark:/67531/metadc58552/m1/1/: accessed November 13, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.