Effect of hard anodize thickness on the fatigue of AA6061 and C355 aluminium

Journal of Materials Science Letters

Volumn 15, Issue 15, 1996, Pages 1321-1323

  Rateick Jr , R G ^a   Binkowski, T C ^b,c   Boray, B C ^b,d  

^a AlliedSignal Aerospace Equipment Systems   (United States)

^b VALPARAISO UNIVERSITY   (United States)

^c UNIVERSITY OF SOUTH CAROLINA   (United States)

^d UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANODIC OXIDATION; COATINGS; CURVE FITTING; FATIGUE OF MATERIALS; FATIGUE TESTING; MATHEMATICAL MODELS; ROUGHNESS MEASUREMENT; STRENGTH OF MATERIALS; SURFACE ROUGHNESS; THICKNESS MEASUREMENT;

ALUMINUM SILICON MAGNESIUM ALLOYS; CURVE FIT RESIDUAL; HARD ANODIZATION; HARD ANODIZE THICKNESS; INTERPOLATED EQUIVALENT STRESS MODEL; KROUSE TESTING; STRESS LIFE CURVES; STYLUS PROFILOMETRY;

ALUMINUM ALLOYS;

EID: 0030215204     PISSN: 02618028     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF00240794     Document Type: Article

References (7)

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2. J. S. ABBOTT, Adv. Mater. Proc. September (1994) 29.
3. "Military specification, anodic coatings, for aluminum and aluminum alloys", MIL-A-8625E, United States Department of Defence, Washington D.C., (1988).
4. Mater. Meth. 32 (1950) 62.
5. "Military handbook, metallic materials and elements for aerospace vehicle structures", MIL-HDBK-5F, United States Department of Defence, Washington D.C., (1992).
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7. F. G. GILLIG, "Study of hard coatings for aluminum alloys", WADC technical report 53-151, May (1953).