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Prediction of endurance limit of hardened parts with account of operational factors
Pavlov V.F., Kirpichev V.A., Kiselev P.E., Shvetsova A.A.
Coefficient of residual stresses influence on cylindrical parts endurance limit under bending estimation
Semyonova O.Y., Kirpichev V.A., Deniskina E.A.
Relation between characyeristics of low-cycle and high-cycle fatigue of threaded parts and residual stresses
Zlobin A.S.
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
Bolotov M.A., Zhidyaev A.N., Surkov O.S.
Estimation of residual stress influence on the low-cycle fatigue of threaded parts
Zlobin A.S.
Methods of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment
Gromakovsky D.G., Kovshov A.G., Kotcherov E.P., Makaryants M.V.
Modification of the surface of silicon carbide parts by laser treatment for improving their tribological properties
Murzin S.P., Balyakin V.B., Zhuravel L.V.
Research of notch radius and depth influence on residual stresses distribution character in the smallest cross-section of surface hardened detail
Sazanov V.P., Larionova Y.S.
The dependence of detail fatigue resistance on the thickness of hardening layer under outstripping superficial plastic deforming
Vakuljuk V.S.
Forecasting the endurance limit of surface-hardened cylindrical parts made of steel 20 by the initial deformations of reference specimen
Sazanov V.P.
Superficial hardened part critical depth of non-propagating fatigue crack evaluation
Kirpichev V.A., Semyonova O.Y.
FMS-3000, programming amilling machine 6M13GN-1 a program controller
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Research of changes in shape and location ring details with small rigidity
Galuzina T.V., Polyakov A.V.
Residual stresses distribution regularities in the smallest section of hardened hollow cylindrical detail with circular cut
Sazanov V.P., Larionova Y.S., Kolychev S.A.
Increase of stability of technological systems at processing of details aircrafts engines
Skuratov D.L., Burmistrov E.V., Samykin V.N.
Aircraft engine design based on unified gas generator
Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.
Study of residual strained state components distribution in the smallest section of superficial hardened part with a circular cut by finite-elements modeling method
Sazanov V.P.
1 - 17 of 17 Items

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