Application of Average Stress Criterion to Fracture of Aluminium Alloys Used in Aerospace Applications

Author:

John H. Brighton Isaac

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference10 articles.

1. Starke Jr. E.A., Staleyt J.T.: Application of modern aluminum alloys to aircraft, Pro 9. Aerospace Sci. 32, 131–172 (1996)

2. Christopher T., Sankaranarayanasamy K., Nageswara Rao B.: Fracture behavior of maraging steel tensile specimens and pressurized cylindrical vessels. Fatigue Fract. Eng. Mater. Struct. 27, 177–186 (2004)

3. Christopher T., Sankaranarayanasamy K., Nageswara Rao B.: Correlating cryogenic fracture strength using a modified two-parameter method. Eng. Fract. Mech. 72, 475–490 (2005)

4. Christopher T., Sankaranarayanasamy K., Nageswara Rao B.: Failure assessment of flawed steel cylinders tested under internal pressure. Steel Grips (J. Steel Relat. Mater.), 3(2), 130–137 (2005)

5. Damage Tolerant Design Handbook: A compilation of Fracture and Crack Growth Data for High Strength Alloys. Metals and Ceramics Information Center, Battelle, Columbus Laboratories, Ohio. Report No. MCIC-HB-01 (January 1975)

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