Old Web
English
Sign In
Acemap
>
Paper
>
Damage tolerant design of critical aircraft structural components
Damage tolerant design of critical aircraft structural components
1992
David Bearden
Bruce Starley
Keywords:
Damage tolerance
Fracture mechanics
Residual stress
Fracture toughness
Crack closure
Forensic engineering
Materials science
Structural engineering
Flexural strength
Structural mechanics
Correction
Source
Cite
Save
Machine Reading By IdeaReader
2
References
0
Citations
NaN
KQI
[]