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NASA-LLIS-0764

Lessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applications

active, Most Current
Organization: NASA
Publication Date: 6 April 2000
Status: active
Page Count: 5
scope:

Practice:

This practice presents considerations that should be evaluated and applied concerning stress corrosion and subsequent crack propagation in mechanical devices, structural devices, and related components used in aerospace applications. Material selection, heat treat methods, fabrication methodology, testing regimes, and loading path assessments are presented as methods to reduce the potential for stress corrosion cracking in a material's operational environment.

Document History

NASA-LLIS-0764
April 6, 2000
Lessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applications
Practice: This practice presents considerations that should be evaluated and applied concerning stress corrosion and subsequent crack propagation in mechanical devices, structural devices, and...

References

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