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Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4
An investigation of the damping-in-roll characteristics of three wings with an aspect ratio of 4, a taper ratio of 0.6, three sweep angles at the quarter chord line, and the NACA 65A006 section as determined through a range of Mach numbers and angles of attack.
Date:
June 27, 1949
Creator:
Kuhn, Richard E. & Myers, Boyd C., II
System:
The UNT Digital Library