28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-2.10.3


THE INVESTIGATION OF A POSSIBILITY OF INCREASING THE LIFT-TO-DRAG RATIO OF A MANEUVERABLE AIRCRAFT AT SUBSONIC SPEEDS

A. A. Pavlenko
TsAGI, Russian Federation

Keywords: maneuverable aircraft, subsonic speed, lift-to-drag ratio, wing mid surface, leading edge flap

Experimentally shown that the L/D increment due to whole wing deformation is 4.53.0, 0.6

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