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 |
On selection of equivalent loading of standard smooth specimens for determining low-cycle durability of gas-turbine engine major components |
(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 optimization of the turbine blade-disk interlock of the type “fir tree” |
(Rus)
|
Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш |
(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 11, No 3-1 (2012): Special Issue |
CONFERENCE MATERIALS |
The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method |
(Rus)
|
Vol 13, No 5-4 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Study of cycle life of a material in conditions of low-cycle fatigue and long-term strength |
(Rus)
|
Vol 13, No 5-4 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation |
(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 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)
|