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Search by keyword: "mathematical modeling"
End window profiling of a trochoid machine
| Authors: Kasko A.A., Zelentsov A.A., Minin V.P. | Published: 19.10.2022 |
| Published in issue: #11(752)/2022 | |
| Category: Energy and Electrical Engineering | Chapter: Heat Engines | |
| Keywords: mathematical modeling, working process, trochoid rotary machine, trochoid compressor |
Digital Twins — a Platform for Aircraft Engine Lifecycle Management
| Authors: Salnikov A.V., Gordin M.V., Shmotin Yu.N., Nikulin A.S., Makarov P.V., Frantsuzov M.S. | Published: 01.04.2022 |
| Published in issue: #4(745)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: digit twin, gas turbine engine, requirement matrix, digital platform, life cycle, mathematical modeling |
Shaping the Combustion Chamber of a Piston Engine with Direct Injection of Gasoline
| Authors: Kavtaradze R.Z., Kasko A.A., Zelentsov A.A. | Published: 23.09.2019 |
| Published in issue: #9(714)/2019 | |
| Category: Energy and Electrical Engineering | Chapter: Heat Engines | |
| Keywords: piston engine, gasoline direct injection, heat transfer, mathematical modeling |
The Results of Numerical Research of High-Temperature Flow Heterogeneity Caused by Edge Wakes of Nozzle Blades with Film Cooling
| Authors: Sidorov A.A., Kiselev S.V., T.V. Polnikova | Published: 24.11.2016 |
| Published in issue: #11(680)/2016 | |
| Category: Transportation and Power Engineering | |
| Keywords: nozzle vane profile, aerodynamic wake, high-temperature flow, cooling of profiles, mathematical modeling |
The Analysis of Influence of the Nozzle Structure and Fluid Injection Path on the Efficiency of Two-Phase Mixing in a Constant Cross Section Channel
| Authors: Arefyev K.Yu., Voronetskiy A.V., Prokhorov A.N., Suchkov S.A., Filimonov L.A. | Published: 30.06.2016 |
| Published in issue: #7(676)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: mathematical modeling, fuel injection, droplet fragmentation, droplet evaporation, constant section channel |
Numerical Analysis of the Thermal State of the Resonator in a Gas-Dynamic Ignition System with Two-Phase Fuel Composition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 11.05.2016 |
| Published in issue: #5(674)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: thermal state, gas-dynamic ignition system, two-phase fuel composition, mathematical modeling, ethanol, temperature field, resonator, pulsed mode |
On the Assessment of Measurement Results and Their Interpretation to Obtain Information on the Operation of Machines and Mechanisms
| Authors: Pronyakin V.I. | Published: 11.05.2016 |
| Published in issue: #5(674)/2016 | |
| Category: Technology and Process Machines | |
| Keywords: phase-chronometric method, precision time measurement, information and metrological support, technical diagnostics, mathematical modeling, defect |
The Application of Cyclic Symmetry and the Substructure Method in the Thermal Stress Analysis of the Combustion Chamber of the Liquid-Propellant Rocket Engine with LOX Cooling
| Authors: Korotkaya O.V., Gavryushin S.S. | Published: 20.01.2016 |
| Published in issue: #1(670)/2016 | |
| Category: Technology and Process Machines | |
| Keywords: mathematical modeling, finite element method, substructure, cyclic symmetry, stress-strain state, nozzle, combustion chamber, liquid-propellant rocket engine, cooling channels, LOX-cooling |
Computer-aided design and analysis of cam gears
| Authors: Leonov I.V. | Published: 02.02.2015 |
| Published in issue: #2(659)/2015 | |
| Category: Calculation and Design of Machinery | |
| Keywords: energy consumption, starting, braking, synthesis of mechanisms, mathematical modeling, kinematic pair of higher degree, cam gear, lifting force |
Study of the thermal state of a resonator in a gas-dynamic system initiating monopropellant decomposition
| Authors: Vorozheeva O.A., Arefyev K.Yu. | Published: 04.07.2014 |
| Published in issue: #7(652)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: gas-dynamic system, thermal state, monopropellant, mathematical modeling |