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Laminar flow control for transport aircraft applicationsThe incorporation of laminar flow control into transport aircraft is discussed. Design concepts for the wing surface panel of laminar flow control transport aircraft are described. The development of small amounts of laminar flow on small commercial transports with natural or hybrid flow control is examined. Techniques for eliminating the insect contamination problem in the leading-edge region are proposed.
Document ID
19870025747
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wagner, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
May 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Accession Number
87A13021
Distribution Limits
Public
Copyright
Other

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