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High lift selected conceptsThe benefits to high lift system maximum life and, alternatively, to high lift system complexity, of applying analytic design and analysis techniques to the design of high lift sections for flight conditions were determined and two high lift sections were designed to flight conditions. The influence of the high lift section on the sizing and economics of a specific energy efficient transport (EET) was clarified using a computerized sizing technique and an existing advanced airplane design data base. The impact of the best design resulting from the design applications studies on EET sizing and economics were evaluated. Flap technology trade studies, climb and descent studies, and augmented stability studies are included along with a description of the baseline high lift system geometry, a calculation of lift and pitching moment when separation is present, and an inverse boundary layer technique for pressure distribution synthesis and optimization.
Document ID
19820007144
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Henderson, M. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1979
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-159093
Report Number: NASA-CR-159093
Accession Number
82N15017
Funding Number(s)
CONTRACT_GRANT: NAS1-14742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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