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Making Large Suction Panels For Laminar-Flow ControlPerforated titanium panels used to identify and resolve issues related to manufacture. Recently, relatively large suction panels with aerodynamically satisfactory surface perforations and with surface contours and smoothness characteristics necessary for Laminar-Flow Control (LFC) designed, fabricated, and tested. Requirements of production lines for commercial transport airplanes carefully considered in development of panels. Sizes of panels representative of what is used on wing of commercial transport airplane. Tests of perforated panels in transonic wind tunnel demonstrated aerodynamic stability at flight mach numbers.
Document ID
19910000069
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Maddalon, Dal V.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
February 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 2
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
LAR-13844
Accession Number
91B10069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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