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Investigation of the edge effect in composites using the ANSYS software in a two-dimensional formulation
Skvortsov Y.V., Evtushenko M.A.
Development of a model for determination of preloads on blade shrouds
Pechenina E.Y., Kudashov E.V., Pechenin V.A.
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.
Modeling non-through surface cracks in the thin-walled structures
Skvortsov Y.V., Glushkov S.V.
Application of simulation modelling in static tests of space-rocket vehicles
Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.
Computer simulation of thin-walled tube sink drawing
Kargin V.R., Kargin B.V., Pastushenko T.S., Yerisov Y.A.
Properties of a multi-layer multi-span corrugated package
Alkeev R.I., Suslikov V.I., Eskin I.D.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Calculation of the performance of a coulomb friction damper of a crown bevel gear wheel for different forms of resonant oscillations
Kozharinov E.V., Temis J.M.
Numerical simulation of separation processes in mechanical working
Ivanov K.M., Vinnik P.M., Ivanov V.N.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Analysis of buckling of supported aircraft module skin under compressive load
1 1., 1 1.
Research of dynamic parameters of hot forging on hammers with freely falling parts
Shitarev I.L., Khaimovich A.I.
Advanced methods for assessing sealing ability of valve seals
Kondrashov Y.I., Sergeev R.N.
Forming the conceptual structure of a dimensionally stable platform by numerical optimization
Peresypkin K.V., Kozhichenkova M.S.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Estimation the factors, make the greatest influence on reliability parametres of a GTD disk with a glance sudden failures
Belousov A.I., Gritsin A.V.
Safety front shock damper (shock absorber) to protect containers in emergency falling
Samokhin P.A., Bakhareva E.A., Potanin D.V.
Method of calculating vibrations in a pipeline with damping supports made of MR material
Bezborodov S.A., Ulanov A.M.
Analysis of the applicability of laser stereolithography technology for the production of turbodrives
Shabliy L.S.
1 - 21 of 21 Items

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