| Issue |
Section |
Title |
File |
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Prognostication of the technological residual deformations of slim disks after strengthening by means of superficial plastic straining |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Automatical system for determination the residual tensions in the segments of complex forms |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The determination of the efficient parameters of surface strenghtening the thin-walled and the small-hard parts of gas turbine engines based on deformation tolerance |
(Rus)
|
| Vol 12, No 3-2 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Dynamic method of investigating stress concentrators of the YMZ-238 engine crankshaft considering surface hardening plastic deformation |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Nitriding influence on residual stresses and endurance limit of specimens with notches made of 38Х2МЮА steel |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Evaluation of thermochemical treatment influence on fatigue strength of specimens under normal and high temperatures |
(Rus)
|
| Vol 13, No 5-1 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Dependence of the endurance limit on the character of residual stresses distribution in the surface layer of hardened parts |
(Rus)
|
| Vol 14, No 3-2 (2015): Special Issue |
ISSUE WITHOUT SECTION |
Calculation methods of investigating the surface layer of thin-walled shafts hardened by methods of surface plastic deformation |
(Rus)
|
| Vol 15, No 3 (2016) |
MECHANICAL ENGINEERING AND POWER ENGINEERING |
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range |
(Rus)
|
| Vol 17, No 2 (2018) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Forecasting low-cycle fatigue life of gas-turbine engine parts by the method of equivalent tests for specimens with stress concentrator under extension-compression |
(Rus)
|
| Vol 17, No 3 (2018) |
MECHANICAL ENGINEERING |
Residual stress optimization of technological processes with the aim of ensuring adhesion of nickel or chromium coatings on parts made of titanium alloys |
(Rus)
|
| Vol 10, No 3-2 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator |
(Rus)
|
| Vol 10, No 3-2 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The development of the optimization methodology of the turbine blade-disk interlock of the type “fir tree” |
(Rus)
|
| Vol 21, No 1 (2022) |
MECHANICAL ENGINEERING |
Strength calculation of parts based on stress state stiffness |
(Rus)
|
