| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A Celebration of the Life of Professor Tony Kelly ScD FRS FREng PhD CBE DL
|
Beaumont, Peter W. R.
|
|
2014
|
21 |
3 |
p. 391-395
|
artikel
|
| 2 |
A Global–Local Numerical Model for the Prediction of Impact Induced Damage in Composite Laminates
|
Riccio, A.
|
|
2013
|
21 |
3 |
p. 457-466
|
artikel
|
| 3 |
A Novel Method for Calculation of Strain Energy Release Rate of Asymmetric Double Cantilever Laminated Composite Beams
|
Shokrieh, M. M.
|
|
2013
|
21 |
3 |
p. 399-415
|
artikel
|
| 4 |
A Practical Tool for the Preliminary Design of Bonded Composite Repairs
|
Riccio, A.
|
|
2013
|
21 |
3 |
p. 495-509
|
artikel
|
| 5 |
Composite Structural Analysis of Flat-Back Shaped Blade for Multi-MW Class Wind Turbine
|
Kim, Soo-Hyun
|
|
2013
|
21 |
3 |
p. 525-539
|
artikel
|
| 6 |
Editorial
|
Beaumont, P. W. R.
|
|
2014
|
21 |
3 |
p. 397
|
artikel
|
| 7 |
Effects of Interphase Damage and Residual Stresses on Mechanical Behavior of Particle Reinforced Metal-Matrix Composites
|
Aghdam, M. M.
|
|
2013
|
21 |
3 |
p. 429-440
|
artikel
|
| 8 |
Holistic and Consistent Design Process for Hollow Structures Based on Braided Textiles and RTM
|
Gnädinger, Florian
|
|
2014
|
21 |
3 |
p. 541-556
|
artikel
|
| 9 |
Innovative Anti Crash Absorber for a Crashworthy Landing Gear
|
Guida, Michele
|
|
2013
|
21 |
3 |
p. 483-494
|
artikel
|
| 10 |
Numerical Simulations of Inter-laminar Damage Evolution in a Composite Wing Box
|
Riccio, A.
|
|
2013
|
21 |
3 |
p. 467-481
|
artikel
|
| 11 |
Ratcheting Assessment of GFRP Composites in Low-Cycle Fatigue Domain
|
Ahmadzadeh, G. R.
|
|
2013
|
21 |
3 |
p. 417-428
|
artikel
|
| 12 |
Simulating the Response of Composite Plates to Fire
|
Riccio, A.
|
|
2013
|
21 |
3 |
p. 511-524
|
artikel
|
| 13 |
Static Tensile and Transient Dynamic Response of Cracked Aluminum Plate Repaired with Composite Patch – Numerical Study
|
Khalili, S. M. R.
|
|
2014
|
21 |
3 |
p. 441-455
|
artikel
|
| 14 |
Three-Dimensional BEM and FEM Submodelling in a Cracked FML Full Scale Aeronautic Panel
|
Citarella, R.
|
|
2014
|
21 |
3 |
p. 557-577
|
artikel
|
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