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Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
Language: en
Pages: 644
Authors: Kenneth P. Spreemann
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or
Aero/space Engineering
Language: en
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Aeronautical Engineering Review
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Aircraft Excrescence Drag
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