Found: 9
Select item for more details and to access through your institution.
The 2012 Structures and Composites Special Issue.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1221, doi. 10.1017/S0001924000007600
- By:
- Publication type:
- Article
Modelling progressive failure of fibre reinforced laminated composites: mesh objective calculations.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1221, doi. 10.1017/S0001924000007612
- By:
- Publication type:
- Article
The perforation resistance of sandwich structures subjected to low velocity projectile impact loading.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1247, doi. 10.1017/S0001924000007624
- By:
- Publication type:
- Article
Computation of stress intensity factors in functionally graded materials using partition-of-unity meshfree method.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1263, doi. 10.1017/S0001924000007636
- By:
- Publication type:
- Article
Finite element modelling of sandwich panels with graded core under various boundary conditions.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1289, doi. 10.1017/S0001924000007648
- By:
- Publication type:
- Article
The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1315, doi. 10.1017/S000192400000765X
- By:
- Publication type:
- Article
A finite element analysis of impact damage in composite laminates.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1331, doi. 10.1017/S0001924000007661
- By:
- Publication type:
- Article
Modelling of impact damage zones in composite laminates for strength after impact.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1349, doi. 10.1017/S0001924000007673
- By:
- Publication type:
- Article
Predicting low-velocity impact damage in composites by a quasi-static load model with cohesive interface elements.
- Published in:
- Aeronautical Journal, 2012, v. 116, n. 1186, p. 1367, doi. 10.1017/S0001924000007685
- By:
- Publication type:
- Article