| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
A model for fatigue crack propagation
|
Antolovich, Stephen D.
|
|
1975
|
7 |
4 |
p. 649-652
4 p.
|
article
|
| 2 |
An infinite row of collinear cracks at the interface of two bonded dissimilar elastic half planes
|
Parihar, K.S.
|
|
1975
|
7 |
4 |
p. 751-759
9 p.
|
article
|
| 3 |
A study of the effects of mechanical and environmental variables on fatigue crack closure
|
Irving, P.E.
|
|
1975
|
7 |
4 |
p. 619-630
12 p.
|
article
|
| 4 |
A unified engineering approach to the prediction of multiaxial fatigue fracture of aircraft structures
|
Toor, Pir M.
|
|
1975
|
7 |
4 |
p. 731-741
11 p.
|
article
|
| 5 |
Comment on contribution on “theory of fatigue crack growth” by G. P. Cherepanov and H. Halmanov
|
Cherepanov, Genady P.
|
|
1975
|
7 |
4 |
p. 771-
1 p.
|
article
|
| 6 |
Comment on ‘on the pressure dependency of threshold stress intensity’ by W.W. Gerberich
|
St-John, C.
|
|
1975
|
7 |
4 |
p. 771-772
2 p.
|
article
|
| 7 |
Crack opening interferometry—The effects of optical refraction
|
Fowlkes, Charless W.
|
|
1975
|
7 |
4 |
p. 689-692
4 p.
|
article
|
| 8 |
Cyclic crack growth and fracture resistance of Ti-6Al-6V-2Sn as influenced by recrystallization anneal and interstitial oxygen content
|
Kondas, K.R.
|
|
1975
|
7 |
4 |
p. 641-644
4 p.
|
article
|
| 9 |
Erratum
|
|
|
1975
|
7 |
4 |
p. 775-
1 p.
|
article
|
| 10 |
Fracture angle and strain-energy-density-factor of a crack at hole at an arbitrary angle
|
Hsu, Y.C.
|
|
1975
|
7 |
4 |
p. 743-750
8 p.
|
article
|
| 11 |
Is fracture mechanics evolving to answer the needs of design and strength substantiation?
|
Barrois, W.
|
|
1975
|
7 |
4 |
p. 767-769
3 p.
|
article
|
| 12 |
Numerical computation of dynamic stress intensity factors by a Lagrangian finite-difference method (the HEMP code)
|
Chen, Y.M.
|
|
1975
|
7 |
4 |
p. 653-660
8 p.
|
article
|
| 13 |
Practical use of the ‘equivalent’ measured stress intensity factor to control fatigue crack propagation rates in aircraft full-scale fatigue tests—First assessment of the method in testing of a pressurized aircraft fuselage
|
Barrois, W.
|
|
1975
|
7 |
4 |
p. 673-680
8 p.
|
article
|
| 14 |
Response to C. St. John's comment
|
Gerberich, William W.
|
|
1975
|
7 |
4 |
p. 772-773
2 p.
|
article
|
| 15 |
The application of the visioplasticity technique for derivation of the criterion for ductile rupture initiation in fully plastic notched bars
|
Mohamed, S.A.
|
|
1975
|
7 |
4 |
p. 631-632
2 p.
|
article
|
| 16 |
The effect of sheet thickness on fatigue crack retardation in 2024-T3 aluminum alloy
|
Mills, W.J.
|
|
1975
|
7 |
4 |
p. 705-708
4 p.
|
article
|
| 17 |
The influence of the stress state on the plastic zone size
|
Aurich, D.
|
|
1975
|
7 |
4 |
p. 761-765
5 p.
|
article
|
| 18 |
The J-integral applied to cyclic loading
|
Lamba, H.S.
|
|
1975
|
7 |
4 |
p. 693-703
11 p.
|
article
|
| 19 |
Thermal stress singularities at tips of a crack in a semi-infinite medium under uniform heat flow
|
Sekine, H.
|
|
1975
|
7 |
4 |
p. 713-729
17 p.
|
article
|
| 20 |
Verification of various methods for fatigue notch effect estimations in case of aircraft materials
|
Buch, Alfred
|
|
1975
|
7 |
4 |
p. 661-671
11 p.
|
article
|
Journal description