FIELD: aircraft equipment.
SUBSTANCE: proposed complex includes supersonic aircraft with elongated wells on its surface whose axes are parallel to airframe axis and armament for suspension in these wells protruding beyond cross sectional area. Cross sectional areas of wells may have the following forms: rectangle, square, trapezium, triangle, equilateral triangle, rhomb or curvilinear triangle. Cross sections of armament have respective form and are so located that interference of shock waves in space between armament and aircraft planes may be eliminated.
EFFECT: reduction of aerodynamic drag.
7 cl, 15 dwg
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