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High-subsonic damping-in-roll characteristics of a wing with the quarter-chord line swept back 35 degrees and with aspect ratio 3 and taper ratio 0.6
Report presenting an investigation of the damping-in-roll characteristics of a 35 degree sweptback wing, with and without vertical fins, through a range of Mach numbers in the high speed 7- by 10-foot tunnel utilizing a free-to-roll technique. The damping-in-roll coefficient increased in magnitude with Mach number in the manner indicated by theory and generally was found to increase in magnitude with angle of attack over the range tested.
Date:
May 10, 1949
Creator:
Myers, Boyd C., II & Kuhn, Richard E.
System:
The UNT Digital Library
Technical Report to the General Advisory Committee
This report provides a discussion of technical activities at the Hanford Works as of May 10, 1949.
Date:
May 10, 1949
Creator:
Greninger, A. B.
System:
The UNT Digital Library