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The Langley 8-ft transonic pressure tunnel laminar-flow-control experimentAn account is given of the considerations involved in selecting the NASA-Langley transonic pressure tunnel's design and test parameters, as well as its liner and a swept wing for laminar flow control (LFC) experimentation. Attention is given to the types and locations of the instrumentation employed. Both slotted and perforated upper surfaces were tested with partial- and full-chord suction; representative results are presented for all.
Document ID
19930057786
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Bobbitt, Percy J.
(NASA Langley Research Center Hampton, VA, United States)
Harvey, William D.
(NASA Langley Research Center Hampton, VA, United States)
Harris, Charles D.
(NASA Langley Research Center Hampton, VA, United States)
Brooks, Cuyler W., Jr.
(NASA Langley Research Center 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
Research And Support Facilities (Air)
Accession Number
93A41783
Distribution Limits
Public
Copyright
Other

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