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Dragging down fuel costsIt has been suggested that modest reductions in friction drag could save U.S. airlines $200-500 million a year. Potentially significant fuel savings are to be expected from laminar flow control (LFC) with suction surfaces on a CTOL subsonic transport; fuel savings from 25 to 40 percent are possible, depending on stage length. NASA has developed advanced computational design tools and methodology, subsonic and transonic NLF (natural laminar flow) and LFC airfoils, practical laminar wing construction techniques, and practical leading-edge treatments applicable to civil and military transports. It is concluded that skin-friction and induced drag approaches can combine to make a 50 percent reduction a reality for commercial and military aircraft of the future.
Document ID
19880033710
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hefner, Jerry N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Publication Information
Publication: Aerospace America
Volume: 26
ISSN: 0740-722X
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ISSN: 0740-722X
Accession Number
88A20937
Distribution Limits
Public
Copyright
Other

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