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Application of Laminar Flow Control Technology to Long-Range Transport DesignThe impact of laminar flow control (LFC) technology on aircraft structural design concepts and systems was discussed and the corresponding benefits were shown in terms of performance and fuel economy. Specific topics discussed include: (1) recent advances in laminar boundary layer development and stability analysis techniques in terms of suction requirements and wing suction surface design; (2) validation of theory and realistic simulation of disturbances and off-design conditions by wind tunnel testing; (3) compatibility of aerodynamic design of airfoils and wings with LFC requirements; (4) structural alternatives involving advanced alloys or composites in combinations made possible by advanced materials processing and manufacturing techniques; (5) addition of suction compressor and drive units and their location on the aircraft; and (6) problems associated with operation of LFC aircraft, including accumulation of insects at low altitudes and environmental considerations.
Document ID
19780019127
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gratzer, L. B.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
George-Falvy, D.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1978
Publication Information
Publication: NASA. Langley Res. Center CTOL Transport Technol., 1978
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78N27070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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