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Tests on an airfoil with two slots suitable for an aircraft of high performance : lift, drag, rolling and yawing moment measurements

机译:对具有两个适用于高性能飞机的槽的翼型进行测试:升力,阻力,滚动和偏航力矩测量

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摘要

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.

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