The design concepts, performance capabilities, and projected applications of the Quiet Short-Haul Research Aircraft (QSRA) are discussed. The propulsive lift system of the QSRA provides the lift required for short field operations at low community noise levels. This system consists of four high bipass ratio, geared turbofan engines mounted so that the engine exhaust flows across the upper surface of the wing (upper surface blowing). Large specially shaped flaps behind each engine control the direction of the flow for each phase of flight. A 95 passenger short haul transport based on this technology could operate out of a 2500 foot runway with a combined takeoff and landing 90 EPNdB footprint area of 2.7 sq mi.
The quiet short-haul research aircraft
1983-02-01
Conference paper
No indication
English
The Quiet Short-haul Research Aircraft (QSRA)
NTRS | 1980
|The Quiet Short-Haul Research Aircraft /QSRA/
NTRS | 1979
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