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QCGAT aircraft/engine design for reduced noise and emissionsThe high bypass ratio QCGAT engine played an important role in shaping the aircraft design. The aircraft which evolved is a sleek, advanced design, six-place aircraft with 3538 kg (7,800 lb) maximum gross weight. It offers a 2778 kilometer (1500 nautical mile) range with cruise speed of 0.5 Mach number and will take-off and land on the vast majority of general aviation airfields. Advanced features include broad application of composite materials and a supercritical wing design with winglets. Full-span fowler flaps were introduced to improve landing capability. Engines are fuselage-mounted with inlets over the wing to provide shielding of fan noise by the wing surfaces. The design objectives, noise, and emission considerations, engine cycle and engine description are discussed as well as specific design features.
Document ID
19800013844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lanson, L.
(Avco Lycoming Div. Stratford, CT, United States)
Terrill, K. M.
(Avco Lycoming Div. Stratford, CT, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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