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 January 19, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.