FIELD: aeronautical engineering. SUBSTANCE: maximum camber of stabilizer profiles from root section to section located at distance from it equal to three thicknesses of fin in zone of conjugation with stabilizer is monotonically changing from 0 to -1 - -2 percent. Then camber is retained to tip of outer wing plane. EFFECT: enhanced aerodynamic efficiency through reduced negative interference drag and circulation distribution in stabilizer span by law close to elliptical. 12 dwg
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