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Operational considerations for laminar flow aircraftConsiderable progress has been made in the development of laminar flow technology for commercial transports during the NASA Aircraft Energy Efficiency (ACEE) laminar flow program. Practical, operational laminar flow control (LFC) systems have been designed, fabricated, and are undergoing flight testing. New materials, fabrication methods, analysis techniques, and design concepts were developed and show much promise. The laminar flow control systems now being flight tested on the NASA Jetstar aircraft are complemented by natural laminar flow flight tests to be accomplished with the F-14 variable-sweep transition flight experiment. An overview of some operational aspects of this exciting program is given.
Document ID
19880014364
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maddalon, Dal V.
(NASA Langley Research Center Hampton, VA, United States)
Wagner, Richard D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Publication Information
Publication: Laminar Flow Aircraft Certification
Subject Category
Aircraft Design, Testing And Performance
Accession Number
88N23748
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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