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Fifty years of laminar flow flight testingLaminar flow flight experiments conducted over the past 50 years are reviewed. The emphasis is on flight testing conducted under the NASA Laminar Flow Control Program, which has been directed towards the most challenging technology application, the high-subsonic-speed transport. The F111/TACT NLF Glove Flight Test, the F-14 Variable-Sweep Transition Flight Experiment, the 757 Wing-Noise Survey and NLF Glove Flight Test, the NASA Jetstar Leading-Edge Flight Test Program, and the recently initiated Hybrid Laminar-Flow-Control Flight Experiment are discussed.
Document ID
19890063984
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wagner, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Maddalon, D. V.
(NASA Langley Research Center Hampton, VA, United States)
Bartlett, D. W.
(NASA Langley Research Center Hampton, VA, United States)
Collier, F. S., Jr.
(High Technology Corp. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 881393
Report Number: SAE PAPER 881393
Meeting Information
Meeting: Aerospace Technology Conference and Exposition
Location: Anaheim, CA
Country: United States
Start Date: October 3, 1988
End Date: October 6, 1988
Accession Number
89A51355
Distribution Limits
Public
Copyright
Other

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