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Progress in propulsion system/airframe structural integrationAttention is given to the improvements in mathematical modeling, and the emerging role of computer-related technology, in airframe structural technology advancements related to the engine/airframe integration requirements of such recent designs as the 747 airliner's JT9D turbofan engine nacelle. Also noted are investigation results concerning propulsion system flight loads and their influence on thrust-specific fuel consumption deterioration, which has been addressed through the development of the novel structural concept of the 'load-carrying core cowl' engine nacelle structure. Analytical studies on integrated system vibration include low frequency, nonsynchronous vibration analyses of large, high bypass turbofan engines that have been conducted by means of three-dimensional integrated finite element models.
Document ID
19830055016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
White, J. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Janssen, T. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Yantis, T. F.
(Boeing Commercial Airplane Co. Seattle, CA, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-1123
Report Number: AIAA PAPER 83-1123
Accession Number
83A36234
Distribution Limits
Public
Copyright
Other

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