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Long-range LFC transportM = 0.83 Laminar Flow Control (LFC) transports, carrying large percentage payloads over a range of 20000 kilometers at cruise L/D's of 39 appear feasible with large space externally braced wings, external fuel pods, active controls, and 70 percent laminar flow on wing and tail surfaces, engine nacelles and struts, and a turbulent fuselage. A combination of a swept-forward inboard and a swept-back outer wing appears superior overall, especially for laminar flow and eliminating leading edge contamination probably caused by flyspecks and ice crystals. Wing divergence appears controllable by a combination of various methods. Wind-mounted superfans with extensive laminar flow on their nacelles appear practical. Their dominant tone noise is below the frequency range of the most strongly amplified TS-waves.
Document ID
19900003192
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pfenninger, Werner
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Publication Information
Publication: NASA, Langley Research Center, Research in Natural Laminar Flow and Laminar-Flow Control, Part 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
90N12508
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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