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Conceptual design study of advanced acoustic-composite nacellesConceptual studies were conducted to assess the impact of incorporating advanced technologies in the nacelles of a current wide-bodied transport and an advanced technology transport. The improvement possible in the areas of fuel consumption, flyover noise levels, airplane weight, manufacturing costs, and airplane operating cost were evaluated for short and long-duct nacelles. Use of composite structures for acoustic duct linings in the fan inlet and exhaust ducts was considered as well as for other nacelle components. For the wide-bodied transport, the use of a long-duct nacelle with an internal mixer nozzle in the primary exhaust showed significant improvement in installed specific fuel consumption and airplane direct operating costs compared to the current short-duct nacelle. The long-duct mixed-flow nacelle is expected to achieve significant reductions in jet noise during takeoff and in turbo-machinery noise during landing approach. Recommendations were made of the technology development needed to achieve the potential fuel conservation and noise reduction benefits.
Document ID
19750021020
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nordstrom, K. E. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Marsh, A. H. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Sargisson, D. F. (GE)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-132703
MDC-J6891
Accession Number
75N29093
Funding Number(s)
CONTRACT_GRANT: NAS1-13356
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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