Maximum lift and longitudinal stability characteristics at Reynolds numbers up to 7.8 x 10(exp 6) of a 35 degree sweptforward wing equipped with high-lift and stall-control devices, fuselage, and horizontal tail
1950-02-09
Miscellaneous
No indication
English
Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections
Online Contents | 2013
|Multielement Airfoil Optimization for Maximum Lift at High Reynolds Numbers
British Library Conference Proceedings | 1991
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