Tracking Potential Crack Growth Damage in U.S. Air Force Aircraft
- 1 July 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (7) , 435-442
- https://doi.org/10.2514/3.58384
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Damage tolerance assessment of F-4 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- DEVELOPING METHODS FOR TRACKING CRACK GROWTH DAMAGE IN AIRCRAFTPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- New Air Force Requirements for Structural Safety, Durability, and Life ManagementJournal of Aircraft, 1976
- Effect of width and length on stress intensity factors of internally cracked plates under various boundary conditionsInternational Journal of Fracture, 1971
- The—S/N—Fatigue-life gage: A direct means of measuring cumulative fatigue damageExperimental Mechanics, 1966