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The Effect of Continuous Weathering on Light Metal Alloys Used in Aircraft (1939)

NASA Technical Reports Server (NTRS) · leaf 24

An illustration from The Effect of Continuous Weathering on Light Metal Alloys Used in Aircraft, 1939, leaf 24
0 a Figure 15.—Representative cross sections showing corrosion on Dowmetal tensile bars 0.5 inch diameter exposed at Hampton Roads for 1 year. The specimens were all given the chrome-pickle surface treatment. Those designated "unattacked" were given additional paint protection. Note the superiority…

NASA Technical Reports Server (NTRS)

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