nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A Comparative Study of Tensile Fracture Mechanisms
|
Mullin, J.V. |
|
1972 |
6 |
2 |
p. 268-276 |
artikel |
2 |
Finite Element Solutions for Laminated Thick Plates
|
Mau, S.T. |
|
1972 |
6 |
2 |
p. 304-311 |
artikel |
3 |
Fracture Mechanics Approach to Adhesive Joints
|
Trantina, G.G. |
|
1972 |
6 |
2 |
p. 192-207 |
artikel |
4 |
Fracture Mechanics of a Fiber Composite
|
Zimmer, J.E. |
|
1972 |
6 |
2 |
p. 312-315 |
artikel |
5 |
Free-Edge Delamination of Tensile Coupons
|
Whitney, J.M. |
|
1972 |
6 |
2 |
p. 300-303 |
artikel |
6 |
Observations of Failure Modes in Carbon Composite Materials
|
Frye, E.R. |
|
1972 |
6 |
2 |
p. 286-292 |
artikel |
7 |
Shear Buckling of an Elastically Supported Fiber
|
Lovell, Edward G. |
|
1972 |
6 |
2 |
p. 296-299 |
artikel |
8 |
Shear Deformation in Heterogeneous Anisotropic Plates
|
Kan, Y.R. |
|
1972 |
6 |
2 |
p. 316-319 |
artikel |
9 |
Stress Pulse Attenuation in Cloth-Laminate Quartz Phenolic
|
Reed, R.P. |
|
1972 |
6 |
2 |
p. 232-257 |
artikel |
10 |
Structure-Property Relations and Reliability Concepts
|
Halpin, John C. |
|
1972 |
6 |
2 |
p. 208-231 |
artikel |
11 |
The Integration of Composite Structures into Aircraft Design
|
Waddoups, M.E. |
|
1972 |
6 |
2 |
p. 174-190 |
artikel |
12 |
Thermal Conductivities Based on Variational Principles
|
Donea, Jean |
|
1972 |
6 |
2 |
p. 262-266 |
artikel |
13 |
The Transverse Poisson's Ratio of Composites
|
Foye, R.L. |
|
1972 |
6 |
2 |
p. 293-295 |
artikel |
14 |
Ultrasonic Wave Propagation in Metal-Matrix Composites
|
Lord, Arthur E. |
|
1972 |
6 |
2 |
p. 278-285 |
artikel |