Investigation of Effects of Leading-Edge Chord-Extensions and Fences in Combination with Leading-Edge Flaps on Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of 45° Sweptback Wing of Aspect Ratio 4.
Investigation of effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on aerodynamic characteristics at mach numbers from 0.40 to 0.93 of 45° sweptback wing of aspect ratio 4
NACA -- Tech Note
1957
45 pages
Aufsatz (Zeitschrift)
Englisch
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