Recent tests conducted in 7 by 10-ft wind tunnel of University of Detroit; slotted flap of 30% chord fitted on Goettingen 398 (modified) airfoil, showing large increase in lift with very small added drag for small flap deflections.
Airfoil fitted with slotted flap
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 3 , n 12
1936
3 pages
Article (Journal)
English
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