| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
An efficient procedure for determining mixed-mode energy release rates in practical problems of delamination
|
Davidson, Barry D.
|
|
1996
|
102-103 |
2-4 |
p. 193-210
18 p.
|
artikel
|
| 2 |
Application of metal laminates to aircraft structures: Prediction of penetration performance
|
Riddle, Robert
|
|
1996
|
102-103 |
2-4 |
p. 173-192
20 p.
|
artikel
|
| 3 |
Applications of the three dimensional finite element alternating method
|
Pipkins, Daniel S.
|
|
1996
|
102-103 |
2-4 |
p. 133-153
21 p.
|
artikel
|
| 4 |
Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints
|
Deng, Xiangyang
|
|
1996
|
102-103 |
2-4 |
p. 101-114
14 p.
|
artikel
|
| 5 |
A systematic design methodology for generating the optimal repairs of aging aircraft
|
Chickermane, Hemant
|
|
1996
|
102-103 |
2-4 |
p. 365-379
15 p.
|
artikel
|
| 6 |
Author index volume 23
|
|
|
1996
|
102-103 |
2-4 |
p. 405-406
2 p.
|
artikel
|
| 7 |
Computational modeling of elastic and plastic multiple cracks by the fundamental solutions
|
Dong, Y.F.
|
|
1996
|
102-103 |
2-4 |
p. 115-132
18 p.
|
artikel
|
| 8 |
Contents volume 23
|
|
|
1996
|
102-103 |
2-4 |
p. 407-408
2 p.
|
artikel
|
| 9 |
Development of a new frame finite element for crash analysis, using a mixed variational principle and rotations as independent variables
|
Vasudevan, S.
|
|
1996
|
102-103 |
2-4 |
p. 155-171
17 p.
|
artikel
|
| 10 |
Editorial
|
|
|
1996
|
102-103 |
2-4 |
p. v-
1 p.
|
artikel
|
| 11 |
Effects of multiple blade interaction on the containment of blade fragments during a rotor failure
|
Sarkar, S.
|
|
1996
|
102-103 |
2-4 |
p. 211-223
13 p.
|
artikel
|
| 12 |
Fracture and fatigue analysis of curved or kinked cracks near fastener holes
|
Chow, W.T.
|
|
1996
|
102-103 |
2-4 |
p. 91-100
10 p.
|
artikel
|
| 13 |
Hybrid simulation strategy for multiple planar collisions with changing topologies and local deformation
|
Ogot, M.
|
|
1996
|
102-103 |
2-4 |
p. 225-239
15 p.
|
artikel
|
| 14 |
Integrated decision support for aviation safety inspectors
|
Luxhøj, James T.
|
|
1996
|
102-103 |
2-4 |
p. 381-403
23 p.
|
artikel
|
| 15 |
Multiaxial constitutive modeling of aircraft engine materials
|
Lu, Z.K.
|
|
1996
|
102-103 |
2-4 |
p. 319-332
14 p.
|
artikel
|
| 16 |
Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires
|
Mc Allen, J.
|
|
1996
|
102-103 |
2-4 |
p. 241-263
23 p.
|
artikel
|
| 17 |
Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires
|
Mc Allen, J.
|
|
1996
|
102-103 |
2-4 |
p. 265-290
26 p.
|
artikel
|
| 18 |
On the feasibility of using thermal gradients for active control of interlaminar stresses in laminated composites
|
Kim, T.
|
|
1996
|
102-103 |
2-4 |
p. 349-363
15 p.
|
artikel
|
| 19 |
The influence of imperfections on the creep behavior of woven polymer composites at elevated temperatures
|
Govindarajan, S.
|
|
1996
|
102-103 |
2-4 |
p. 333-347
15 p.
|
artikel
|
| 20 |
Vibration monitoring of cylindrical shells using piezoelectric sensors
|
Callahan, J.
|
|
1996
|
102-103 |
2-4 |
p. 303-318
16 p.
|
artikel
|
| 21 |
Waves in periodic structures with imperfections
|
Benaroya, H.
|
|
1996
|
102-103 |
2-4 |
p. 291-302
12 p.
|
artikel
|
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