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Comparison of Stress Corrosion Cracking Properties of Several Aircraft Structural Alloys
Language: en
Pages: 9
Authors: JT. Ryder
Categories: Alloys
Type: BOOK - Published: 1978 - Publisher:

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Sustained load subcritical flaw growth characteristics of five alloys of interest to aircraft designers were investigated. The aluminum alloy (2024-T851) and st
Stress Corrosion Cracking in Aircraft Structural Materials
Language: en
Pages: 138
Authors: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel
Categories: Airframes
Type: BOOK - Published: 1967 - Publisher:

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Environmental and Metallurgical Factors of Stress-corrosion Cracking in High-strength Steels
Language: en
Pages: 50
Authors: C. J. Slunder
Categories: Steel, High strength
Type: BOOK - Published: 1961 - Publisher:

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Aluminum-Lithium Alloys
Language: en
Pages: 42
Authors: R.J.H. Wanhill
Categories: Technology & Engineering
Type: BOOK - Published: 2013-09-20 - Publisher: Elsevier Inc. Chapters

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The material and manufacturing property requirements for selection and application of 3rd generation aluminium-lithium (Al–Li) alloys in aircraft and spacecra
Stress-corrosion Cracking in High Strength Steels and in Titanium and Aluminum Alloys
Language: en
Pages: 388
Authors: Benjamin Floyd Brown
Categories: Aluminum alloys
Type: BOOK - Published: 1972 - Publisher:

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