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The use of light aluminum–lithium alloys with high elastic moduli in hybrid laminated materials for the production of skin panels in airplane wings is considered. Click to show full abstract
The use of light aluminum–lithium alloys with high elastic moduli in hybrid laminated materials for the production of skin panels in airplane wings is considered.
Keywords:
fatigue crack;
materials slow;
hybrid laminated;
laminated materials;
slow fatigue;
crack development
Journal Title: Russian Engineering Research
Year Published: 2017
Link to full text (if available)
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Journal Title: Russian Engineering Research
Year Published: 2017
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!