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Laminar flow control SPF/08 feasibility demonstrationThe feasibility of applying superplastic forming/diffusion bonding (SPF/DB) technology to laminar flow control (LFC) system concepts was demonstrated. Procedures were developed to produce smooth, flat titanium panels, using thin -0.016 inch sheets, meeting LFC surface smoothness requirements. Two large panels 28 x 28 inches were fabricated as final demonstration articles. The first was flat on the top and bottom sides demonstrating the capability of the tooling and the forming and diffusion bonding procedures to produce flat, defect free surfaces. The second panel was configurated for LFC porous panel treatment by forming channels with dimpled projections on the top side. The projections were machined away leaving holes extending into the panel. A perforated titanium sheet was adhesively bonded over this surface to complete the LFC demonstration panel. The final surface was considered flat enough to meet LFC requirements for a jet transport aircraft in cruising flight.
Document ID
19820013658
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ecklund, R. C.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Williams, N. R.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-165818
NAS 1.26:165818
Report Number: NASA-CR-165818
Report Number: NAS 1.26:165818
Accession Number
82N21532
Funding Number(s)
CONTRACT_GRANT: NAS1-16425
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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