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Experienceof CAE/CAD-systems using at designing of internal combustion engine
Gorshkalev A.A., Krivtsov A.V., Saigakov E.A., Smorkalov D.V., Uglanov D.A.
Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber
Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.
Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process
Matveev V.N., Goriachkin E.S., Popov G.M., Baturin O.V., Kudryashov I.A.
Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor
Panchenko S.L., Gras’ko T.V.
Main results of use CAE/CAD-systems in the process of design and calculation of the working processes in internal combustion engine
Biryuk V.V., Uglanov D.A., Kayukov S.S., Gorshkalev A.A., Vakarchuk A.A., Burdanov A.M.
Construction and calculation of three-dimensional model threedimensional model of ice combustion chamber for dynamic calculation of heat processes in ANSYS Fluent
Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Uglanov D.A.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Investigation of the influence of non-axisymmetric elements in secondary air system on gas turbine engine flow parameters, the temperature field and deformation of components
Tisarev A.Y., Vasilevich N.M.
Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body
Didenko A.A., Sokolov A.B.
Determination of aircraft part masses based on a parametric 3D model at the stage of technical proposals
Borgest N.M., Gromov A.A., Tarabaeva A.I.
Application CAD/CAE-systems for calculation on durability of details crank rod mechanism of internal combustion engine
Gorshkalev A.A., Krivtsov A.V., Saigakov E.A., Smorkalov D.V.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers
Maksimov A.D., Shustov S.A.
Aircraft engine design based on unified gas generator
Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.
Calculation and experimental investigations on the efficiency of various ways of vibration damping of jet engine parts
Shorr B.F., Serebryakov N.N., Stadnikov A.N., Shadrin D.C., Rudenok E.S., Kanackin A.V., Bortnikov A.D.
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
Tkachenko A.Y., Krupenich I.N.
Numerical investigation multifuel combustion gas turbine combustion chamber module
Malygina M.V.
Reconstruction of fan blade dynamic loading prior to its fracture
Artamonov M.A., Govorov A.A., Starshinov D.S.
Training for innovative engineering through through parametrization
Balyakin V.B., Ermakov A.I., Chempinsky L.A.
Calculation methodology of intermittent burning chamber main parameters
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Calculation of cutting temperature at milling of purveyances from hard-processing materials
Trusov V.N., Skuratov D.L., Zakonov O.I., Shikin V.V.
Development of a methodology for calculating the working process of a small-size two-stroke internal combustion engine
Biryuk V.V., Gorshkalev A.A., Zakharov M.O., Larin V.L.
Mixing processe research in 10…15 N thrusters
Salich V.L., Semkin E.V.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Reduction of circumferential variation in the final stage of IPC
Popov G.M., Mamedov A.C., Smirnova Y.D.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
Calculating the dynamic error in measurement of electrohydromechanical system parameters, taking into account the operating speed of sensors
Gareyev A.M., Gimadiev A.G., Stadnik D.M., Popelnyuk I.A.
Gas dynamic calculation of detonation in variable cross-section ducts
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
Accuracy control method for space complex products at the stage of design engineering
Yelenev V.D., Shuplyak Y.P.
Resonant method of accelerating non-magnetic materials
Syomkin N.D., Piyakov A.V., Voronov K.Y., Sukhachev K.I.
Design of led spotlight secondary optics producing required irradiance distribution
Belousov A.A., Moiseev M.A.
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.
Development of a multiuser system web-interface as a tool of using mathematical packages for solving engineering tasks
Danilenko A.N., Zhdanov I.A.
Analysis of models of fuel elements while using of surface mountng
Knyazeva G.N., Krasnoshchekova G.F., Tyulevin S.V.
Determination of parameters of pulse-magnetic forming
Karpuhin V.F.
Methods of calculating the load characteristics of ring dampers of the MR material with partial coverage of a bearing with precessional loading
Parovay F.V., Ponomaryov Y.K., Kotov A.S., Spivak S.E., Vasyukov E.S.
Gas dynamic calculation of detonation in constant-cross-section ducts
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Combined calculation of gas generators of small GTE in package ANSYS CFX
Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.
Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
Shustov S.A.
Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials
Krivonogov A.V.
1 - 42 of 42 Items

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