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Investigation of Buckling Behavior for Thin-Walled Bearing Aircraft Structural Elements with Cutouts by Means of Numerical Simulation
Dmitriev V.G., Egorova O.V., Zhavoronok S.I., Rabinskii L.N.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
Zheleznov L.P., Kabanov V.V., Boiko D.V.
Nonlinear deforming of laminated composite shells of revolution under finite deflections and normal’s rotation angles
Dmitriev V.G., Biryukov V.I., Egorova O.V., Zhavoronok S.I., Rabinskii L.N.
Study of thin-walled parts shaping process based on flanging and embossing
Dem’yanenko E.G., Popov I.P.
Analytical Evaluation of Box Wing Aircraft Aerodynamic Characteristics at Early Design Stages
Karpovich E.A., Liseitsev N.K.
Analysis of cleaning technology for gas turbine engine oil systems as a stage of product life cycle
Tuktamysheva Y.A., Tuktamyshev V.R.
Collapse of a spheroidal cavitation bubble near a solid wall
Aganin A.A., Il’gamov M.A., Kosolapova L.A., Malakhov V.G.
About Optimal Reception of Pseudorandom Signals of Nonlinear Dynamic Systems
Nasyrov I.K., Andreev V.V.
A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis
Rybakov V.N., Kuz’michev V.S., Tkachenko A.Y., Krupenich I.N.
Analysis of structural elements made of composite materials with defects
Kokurov A.M., Odintsev I.N.
Numerical Estimation of Weight Efficiency for Aircraft Composite Lattice Shells with Grid Parameter Variable over Height
Bokuchava P.N., Evstaf’ev V.A., Babuk V.A.
Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Kornev A.V., Sereda V.A., Migalin K.V.
Analytical and asymptotic solution of boundary value problems in the mechanics of deformed shells under concentrated loading
Bakulin V.N., Vinogradov Y.I.
Optimal Estimation of Parameters of Pseudorandom Signals of Nonlinear Dynamic Systems
Nasyrov I.K., Andreev V.V.
Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending
Belov V.K., Zheleznov L.P., Ognyanova T.S.
Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
Kuz’mina K.S., Marchevskii I.K., Moreva V.S., Ryatina E.P.
A Method for Express Analysis of Mechanical, Erosion, and Contaminating Impact of Plasma Jet of Electric Propulsion Thruster onto the Large Object of Space Debris
Blyakharskii S.S., Blyakharskii Y.S., Nadiradze A.B., Rakhmatullin R.R.
The Interaction Potential of Molecules in Multicomponent Gaseous Media
Anisimova I.V., Ignat’ev V.N., Gortyshov Y.F., Aristova E.Y.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A.V., Azimov R.A., Bukatyi S.A.
Methods for measuring the geometric parameters of products by the laser coordinate measuring system in modern mechanical production
Lyudogovskii P.L., Komkova M.A.
An Integral Method of Surface Damping of Bending Vibrations for Thin-Walled Structures
Paimushin V.N., Firsov V.A., Shishkin V.M.
Study of the Local Strength of the Main Rotor Torsion Bar under the Action of Flight and Test Bench Loads
Mitryaikin V.I., Shuvalov V.A.
Application of a discrete-continuous model of strength analysis to solve the identification problem of a thermally loaded structure
Kostin V.A., Huang S., Valitova N.L.
Stress–strain analysis of a thin-shell part of fuselage using a triangular finite element with lagrange multipliers
Klochkov Y.V., Nikolaev A.P., Vakhnina O.V., Kiseleva T.A.
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