SUPERSONIC AIRCRAFT Russian patent published in 1997 - IPC

FIELD: aircraft manufacture. SUBSTANCE: aircraft fuselage is smoothly engageable with wing and with upper portion of engine nacelle and does not extend beyond engine nozzles which are arranged in single nacelle. Air intakes are located under wing and their leading edges are located at distance equal to 0.6-0.8 of fuselage length counting from its tip. Each half of wing consists of three sections each which has its own span and sweepback of leading edge. Amount of root chord of wing is equal to 0.8-1.0 of fuselage length. Engine air intakes may be with fixed angle of compression wedge. EFFECT: enhanced reliability. 2 cl, 2 dwg