RATE EFFECTS ON RESIDUAL STRENGTH OF FLAWED STRUCTURES AND MATERIALS
The literature is reviewed with respect to tests conducted to investigate crack re-initiation under dynamic loads and arrest of a running crack; metallurgical sources of rate effects; available data for aerospace engineering materials; and mechanical sources of rate effects, dynamic crack tip stresses and kinetic energy effects. Conclusions are drawn and recommendations made.
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Corporate Authors:
National Aerospace Laboratory, Netherlands
Structures and Materials Division
Amsterdam, Netherlands -
Authors:
- Vanleeuwen, H P
- Schra, L
- Publication Date: 1975-12-22
Media Info
- Pagination: 81 p.
Subject/Index Terms
- TRT Terms: Aerospace engineering; Aluminum alloys; Cracking; Dynamic loads; Fatigue tests; Fracture mechanics; Fracture properties; High strength steel; Loads; Materials; Polymers; Residual strength; Residual stress; Strain (Mechanics); Titanium alloys; Yield strength
- Uncontrolled Terms: Crack initiation; Crack propagation; Loading rate; Strain rate
- Old TRIS Terms: Airframe materials
- Subject Areas: Aviation; Materials; Vehicles and Equipment;
Filing Info
- Accession Number: 00169063
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: NLR-TR-76004-U
- Contract Numbers: LI/LW/4969
- Files: TRIS
- Created Date: Jan 30 1978 12:00AM