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NASA refan program statusThe objective of the refan program is to demonstrate the technical feasibility of substantially reducing the noise levels of existing JT8D powered aircraft. The program consists of the design, manufacturing and testing of the refan engines and modified nacelles and airplanes. Experimental testing was completed for the refan engine both at sea level and at altitude conditions. Ground testing for the B727 side- and center-engine installations and flight testing of the DC-9 with refan engines and acoustic nacelles were performed. Preliminary results presented show that substantial noise reductions were achieved.
Document ID
19750015498
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abdalla, K. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Yuska, J. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-71705
Report Number: NASA-TM-X-71705
Meeting Information
Meeting: Air Transportation Meeting
Location: Hartford, CT
Country: United States
Start Date: May 6, 1975
End Date: May 8, 1975
Sponsors: Soc. of Automotive Eng.
Accession Number
75N23570
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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