TITLE

F-16XL to test SLFC wing design

PUB. DATE
November 1994
SOURCE
Aviation Week & Space Technology;11/14/1994, Vol. 141 Issue 20, p52
SOURCE TYPE
Trade Publication
DOC. TYPE
Article
ABSTRACT
Reports on NASA-Langley Research Center's evaluation of an advanced wing design as part of its Supersonic Laminar Flow Control (SLFC) program being conducted in collaboration with the air transport industry. Modification of the left wing to test SLFC concepts designed to reduce boundary layer drag.
ACCESSION #
9411296681

 

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