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Laminar flow flight experiments - A reviewA development history is presented for flight tests of flow-laminarizing technologies, from the wooden-structure wing glove used with the B-18 of about 1940 to the X-21 of 1963-1965 and the wing incidence-varying tests conducted with gloved-wing F-111 and F-14 variable-sweep aircraft in more recent years. Natural laminar flight control testing has also been conducted with a B 757 airliner. Over the years, increasing attention has been given to the treatment of the leading edge of laminar flow wings in order to prevent flow instabilities that precipitate flow transition to turbulence farther aft.
Document ID
19930057781
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
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.
(NASA Langley Research Center Hampton, VA, United States)
Braslow, A. L.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Natural laminar flow and laminar flow control (A93-41776 17-02)
Publisher: Springer-Verlag
Subject Category
Aircraft Design, Testing And Performance
Accession Number
93A41778
Distribution Limits
Public
Copyright
Other

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