Fracture damage of integrated composite joint for fuselage structure under tensile loading
In order to solve the complex load transfer and structural design of the joint structures including skin, longeron and frame in the composite fuselage, the adhesively bonded integrated composite joint was designed. Static tensile test was performed and the strain-load curves and damage modes were ob...
| Format: | Article |
|---|---|
| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2021-08-01
|
| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/04/jnwpu2021394p739/jnwpu2021394p739.html |