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LANN wing designThe LANN wing is the result of a joint effort between Lockheed, the Air Force, NASA, and the Netherlands to measure unsteady pressures at transonic speeds. It is a moderate-aspect-ratio transport wing configuration. The wing was machined from NITRONIC 40 and has 12 percent thick supercritical airfoil sections.
Document ID
19830010484
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Firth, G. C. (Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Langley Research Center Cryogenic Wind Tunnel Models
Subject Category
Research And Support Facilities (Air)
Accession Number
83N18755
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19830010477Collected WorksCryogenic Wind Tunnel Models. Design and Fabrication
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