摘要 |
The heavy lift aircraft has a tandem wings, with the rear wing being of the butterfly type (dihedral, angle greater than 20 degree), and a overpressure obtained under the hull of the catamaran-type fuselage by the diverted feeding of a flow of cold air originating from the fan of the turbofan placed in front of the aircraft, with braking flow at the rear exit by a blocking mobile vane placed between the two fins of the fuselage.
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