A PROCEDURE TO MINIMISE ERROR IN FATIGUE CRACK GROWTH TESTING
β Scribed by M. Oore
- Book ID
- 109013676
- Publisher
- John Wiley and Sons
- Year
- 2007
- Tongue
- English
- Weight
- 657 KB
- Volume
- 18
- Category
- Article
- ISSN
- 8756-758X
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Ahstraet-A crack-o~n~~splacern~t (COD) technique has been successfuity employed to measure crack length in compact tension specimens for the ~te~~t~ of fatigue crack growth rate (FCGR). Details of the COD calibration and comparisons of COD-determined FCGR data with previously established trend lines
Metal fatigue plays a major role in the design of optimised flight vehicles. Economics dictate that modern air vehicles be optimised for weight to maximise performance, therefore an ability to accurately design against the possibility of fatigue failures is paramount. An essential element of the air