The results that are described in this article form a complete series of tests on an airfoil fitted with front and rear slots, the rear slot being formed between the portion of the wing aft of the rear spar and the forward portion of the flap.
Tests on an Airfoil with Two Slots Suitable for an Aircraft of High Performance : Lift, Drag, Rolling and Yawing Moment Measurements
1926-07-01
Sonstige
Keine Angabe
Englisch
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