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Evaluation of laminar flow control system concepts for subsonic commercial transport aircraftA two-year study conducted to establish a basis for industry decisions on the application of laminar flow control (LFC) to future commercial transports was presented. Areas of investigation included: (1) mission definition and baseline selection; (2) concepts evaluations; and (3) LFC transport configuration selection and component design. The development and evaluation of competing design concepts was conducted in the areas of aerodynamics, structures and materials, and systems. The results of supporting wind tunnel and laboratory testing on a full-scale LFC wing panel, suction surface opening concepts and structural samples were included. A final LFC transport was configured in incorporating the results of concept evaluation studies and potential performance improvements were assessed. Remaining problems together with recommendations for future research are discussed.
Document ID
19790007771
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
December 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D6-47109
NASA-CR-158976
Report Number: D6-47109
Report Number: NASA-CR-158976
Accession Number
79N15942
Funding Number(s)
CONTRACT_GRANT: NAS1-14630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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