Fatigue of Aircraft Structures | |
Preparation of Samples used in Fatigue Testing of Aircraft Materials | |
关键词: mechanical processing; stress measurement; X-ray diffraction; | |
DOI : 10.1515/fas-2015-0011 | |
学科分类:航空航天科学 | |
来源: Instytut Lotnictwa / The Institute of Aviation | |
【 摘 要 】
The application of a new type of alloy requires the evaluation of its properties, which is typically achieved with destructive methods. For this purpose, among others, static and fatigue mechanical tests are performed. Tests are performed on standardized samples in a way which reflects the level of stress occurring in real elements. These tests should limit random errors associated with sample preparation. For this reason the proper preparation of samples is crucial, not only in terms of their geometric dimensions but also in terms of the residual stress level. A sample preparation process was developed, involving checking samplesâ surface for cracks, scratches, roughness, and the state of stress. The measurements are performed with nondestructive methods so as not to affect the proceeding research.
【 授权许可】
Unknown
【 预 览 】
Files | Size | Format | View |
---|---|---|---|
RO201904282182411ZK.pdf | 317KB | download |