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Authors
Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft
Volotsuev V.V.
Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions
Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.
Theoretical aspects of designing the components of an aircraft onboard cable network
Myasnikov A.Y.
Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module
Russkikh A.S., Salmin V.V.
Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models
Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.
Selection of aerodynamic characteristics and engine parameters of a maneuverable aircraft under epistemic uncertainty
Veresnikov G.S., Ogorodnikov O.V.
Reliability-oriented design of PCM thermodimensionally stable space structures
Klimakova L.A.
Sales training methods based on through the use of CAD / CAM / CAE systems for aero engines
Balyakin A.V., Ermakov A.I., Pronichev N.D., Chempinsky L.A.
System design of follow shearing dies for cutting sheet blank
Pochekuev E.N., Skripachev A.V., Shenberger P.N.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Analysis of the experience of preparing the users machine-building CAD in centre of the computer designing
Cherepashkov A.A.
Practical application of the methodology of mature production process for pitomated work flow management technology
Puzakina E.J., Larin S.N.
Experience of the deployment the CAD-complex at the educational virtual enterprise
Cherepashkov A.A., Bukatin A.V.
Theory and methods of designing machines with reduced vibroloading
Vasilyev A.V., Gleyzer A.I., Dmitriyev V.N., Prasolov S.G.
Mathematical model of sequential feeders for centralized lubrication systems
Rybaltchenko D.Y., Shakhmatov Y.V., Belov G.O., Ilyukhin V.N.
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder
Komarov V.A., Kutsevich K.E., Pavlova S.A., Tyumeneva T.Y.
Analysis and ballistics design of a laboratory installation system a small calibre with a joined drive on chambers
Safronov A.I., Zorkin V.A., Potapenko V.V.
Introduction of model-based approach to design aircraft
Agaphonov O.A., Vakhrushev D.E., Pryadko S.P., Schukin A.V.
Modern approach for design management in production enterprise integrated information space
Ivaschenko A.V., Kremenetskaya M.E., Filatov A.N., Peisakhovich D.G.
Methodology of the adaptive graphic and geometric training for the computer aided design teaching
1 1.
Optimal design of an induction heater of minimum length
Mednikova V.A.
Conceptual framework of designing complex bundles of aircraft on-board cable network
Koptev A.N., Myasnikov A.Y.
Сhoice of materials for producing dimensionally stable load-carrying structures
Bitkin V.E., Zhidkova O.G., Komarov V.A.
Automated construction of a 3D plane model at the stage of technical proposals
Borgest N.M., Aleev R.H., Aksanian P.A., Gromov A.A.
Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Conception of the student work place arrengement for the computer aided design base teaching
1 1., 1 1.
Modeling direct fuel injection by a multipin nozzle into the ice combustion chamber using CAE/CAD-systems
Biryuk V.V., Kayukov S.S., Gorshkalev A.A., Uglanov D.A., Lysenko Y.D., Zvyagintsev V.A.
Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems
Ryzhkov V.V., Morozov I.I., Lapshin E.A.
Development of small satellite structure taking into account the use of laser measuring systems
Shaposhnikov S.N.
Volume and mass mathematical models of single-stage centripetal ultralow power turbines
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.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.
Calculation of durability of working section of progressive divider valve by a method of final elements
1 1., 1 1., 1 1.
Assessing the strain-stress state parameters of cutting tools and parts during machining
Stepanov A.A., Haimovich A.I.
Artificial intelligence in aircraft design and the role of professor V.G. Maslov’s scientific school in the process of its development
Borgest N.M., Grigoriev V.A., Kuzmichev V.S.
Development of ordinary harness for aircraft onboard cable networks
Koptev A.N., Myasnikov A.Y.
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes
Kornev A.V., Boychuk I.P.
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.
Automated selection of cooling system for radio electronic design of thermophysical
Goryachev N.V., Trusov V.A., Yurkov N.K.
Features of designing gas turbine of complex cycle GT24
1 1.
Forming the conceptual structure of a dimensionally stable platform by numerical optimization
Peresypkin K.V., Kozhichenkova M.S.
Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity
Aleksandrov Y.B., Nguyen T.D., Mingazov B.G.
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.
Design and technical characteristics of transport airplane for arctic exploration
Kuprikov N.V., Dolgov O.S., Kuprikov M.Y., Ivanov B.V.
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system
Kuzmichev V.S., Krupenich I.N., Tkachenko A.Y.
GTE parts optimal design
Temis Y.M., Yakushev D.A.
Features of the new gas turbine aviation engines theory course
Mingazov B.G., Kosterin V.A., Varsegov V.L.
Optimal design of sandwich floor panels made of high-strength composite materials considering stiffness constraints
Komarov V.A., Pavlova S.A.
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.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Hierarchical and associative relations between the terms in the thesaurus in a designer’s dictionary taken as an example
Borgest N.M., Shustova D.V., Gimatdinova S.R.
Problems of unmanned spacecraft reengineering in abnormal flight situations and their knowledge-based solutions
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Analysis and ballistics project the gun tube system with a joined drive on chamber
Safronov A.I., Potapenko V.V.
Digital design of heat-resistant dimensionally stable carbon laminate (CFRP) structures
Komarov V.A., Kishov E.A., Laikova O.G., Pavlov A.A.
Development of methods of modeling and computer aided design of gas turbine engines
Krivosheev I.A., Kozhinov D.G.
Model for the estimation of design work acceleration by parallelization of iterative process in research-intensive mechanical engineering
Komarov V.A., Kremenetskaya M.Y., Sologub A.V., Filatov A.N.
Friction control on changing parameters of friction pairs using sequential feeders
Rybaltchenko D.Y., Bystrov N.D.
1 - 56 of 56 Items

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