Preliminary investigation of spoiler lateral control on a 42 degree sweptback wing at transonic speeds
Description:
Investigation at transonic speeds in the high-speed 7- by 10-foot tunnel to determine the rolling-effectiveness characteristics of a spoiler on a double-wedge-type semispan wing with a sweepback angle of 42 degrees. Results regarding the variation of rolling-moment coefficient, spoiler effectiveness, and rolling effectiveness are provided.
Date:
August 12, 1947
Creator:
Schneiter, Leslie E. & Ziff, Howard L.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department