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Advanced turboprop cargo aircraft systems studyParametric studies were conducted to define the effects of advanced propeller (propfan) characteristics on aircraft direct operating costs, fuel consumption, and noiseprints. Selected propfan aircraft realized 21-percent fuel savings and 15-percent lower DOCs relative to advanced turbofan aircraft. While both the propfan and turbofan aircraft satisfied current federal noise regulations, the propfan aircraft had smaller noiseprints at 90-EPNdB noise levels but larger noiseprints at lower noise levels. Several techniques for reducing the propfan aircraft noiseprints were explored; some of these contribute substantial reductions in noiseprint areas. Also, a propfan aircraft for the C-X role was studied.
Document ID
19810058752
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Muehlbauer, J. C.
(Lockheed-Georgia Co. Marietta, GA, United States)
Morris, S. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-1684
Report Number: AIAA PAPER 81-1684
Meeting Information
Meeting: Aircraft Systems and Technology Conference
Location: Dayton, OH
Start Date: August 11, 1981
End Date: August 13, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A43156
Distribution Limits
Public
Copyright
Other

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