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Selected advanced aerodynamic and active control concepts developmentA summary is presented of results obtained during analysis, design and test activities on six selected technical tasks directed at exploratory improvement of fuel efficiency for new and derivative transports. The work included investigations into the potential offered by natural laminar flow, improved surface coatings and advanced high lift concepts. Similar investigations covering optimum low-energy flight path control, integrated application of active controls and evaluation of primary flight control systems reliability and maintenance are also summarized. Recommendations are included for future work needed to exploit potential advancements.
Document ID
19820007160
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D6-46705
NASA-CR-3220
Report Number: D6-46705
Report Number: NASA-CR-3220
Accession Number
82N15033
Funding Number(s)
CONTRACT_GRANT: NAS1-14742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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