MULTIMODE HIGH MANEUVERABILITY AIRCRAFT OF INTEGRAL AERODYNAMIC CONFIGURATION

摘要

FIELD: aircraft engineering. ^ SUBSTANCE: proposed aircraft comprises airframe wherein central part 2 smoothly fairs with backswept outer wings 3, nose part 1 and tail part 6 wherein all-moving vertical tail 4 and horizontal tail 5 are arranged. Canopy 10 is arranged in airframe hose 1. Airframe features greater width in cross section and is made up of aerodynamic profiles with their height allowing accommodating freight compartment between air intakes. ^ EFFECT: uniform distribution of air load and increased load bearing qualities of airframe. ^ 10 dwg