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Strength and Thermal Limitations of Materials for Airframe Components Lockheed Aircraft Corporation
- Format:
- Conference/Event
- Author/Creator:
- Ekvall, J. C., author.
- Conference Name:
- SAE Southern California Section
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1959
- Summary:
- THE PROPERTIES of presently available and advanced development alloys are reviewed in each of the following groups: (1) magnesium alloys, (2) aluminum alloys, (3) titanium alloys, (4) low-alloy steels, (5) corrosion resistant steels, and (6) nickel, cobalt, and mixed-base alloys.The strongest materials in each group are selected to make comparisons of the strength of typical airframe components at various temperatures. From these comparisons, material-efficiency curves are made to show the strength and thermal limitations of each material group
- Notes:
- Vendor supplied data
- Publisher Number:
- 590067
- Access Restriction:
- Restricted for use by site license
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