Exposure Tests of Galvanized-steel-stitched Aluminum Alloys PDF Download
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Author: Fred M. Reinhart
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 30
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Book Description
Sheets of 24S-T3 and alclade 24S-T3 aluminum alloys joined to themselves by stitching with galvanized steel wire were exposed to a marine atmosphere and in the tidewater to determine whether they would have a satisfactory service life in these environments. Both alloys joined by this method are satisfactory with respect to corrosion resistance for service in marine atmospheres. The alclad 24S-T3 alloy is satisfactory for short periods of time, where the installation is subject to frequent wetting by sea water. The use of 24S-T3 sheet joined by stitching with galvanized wire is not satisfactory when subject to wetting by sea water.
Author: Fred M. Reinhart
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 30
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Book Description
Sheets of 24S-T3 and alclade 24S-T3 aluminum alloys joined to themselves by stitching with galvanized steel wire were exposed to a marine atmosphere and in the tidewater to determine whether they would have a satisfactory service life in these environments. Both alloys joined by this method are satisfactory with respect to corrosion resistance for service in marine atmospheres. The alclad 24S-T3 alloy is satisfactory for short periods of time, where the installation is subject to frequent wetting by sea water. The use of 24S-T3 sheet joined by stitching with galvanized wire is not satisfactory when subject to wetting by sea water.
Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1082
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Author: Maurice Tucker
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 686
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An analytical method is presented for obtaining turbulent temperature recovery factors for a thermally insulated surface in supersonic flow. The method is an extension of Squire's analysis for incompressible flow. The boundary layer velocity profile is represented by a power law and a similarity is postulated for squared-velocity the static-temperature-difference profiles.
Author:
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ISBN:
Category : Science
Languages : en
Pages : 486
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1462
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1464
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 500
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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