Results of tests completed at University of Detroit 7 by 10-ft wind tunnel to determine effects of double split flap dive brakes on lift, drag, and pitching moment characteristics of airfoil and airplane model. Before Inst Aeronautical Sciences.
Effect of dive brakes on airfoil and airplane characteristics
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 11 , n 3
1944
7 pages
Article (Journal)
English
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