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| Topic: |
Technology
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| Number of pages / Number of words: |
4 / 1076 |
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The trailing-edge flap is one method of accomplishing this. The maximum lift coefficient for an airfoil with a simple flap is greater than that for the unflapped airfoil. Also, the coefficients of lift are increased over the entire angle-of-attack range. The stall angle for an airfoil with a simple flap is essentially unchanged from that of the unflapped airfoil...
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The stall angle for an airfoil with a simple flap is essentially unchanged from that of the unflapped airfoil. This is opposed to the slot operation where a higher stall angle was obtained. The flapped airfoil reduces the disadvantage that the slot has in high landing angles.
A Fowler flap is hinged so that it can move back and increase the airplane wing area...
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