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Measurment procedure optimizing geometrical parameters of measure GTE feature on coordinate measuring machine
Bolotov M.A., Cheveleva A.O., Zhidyaev A.N.
Problems of design analysis of characteristics of a gas turbine engine working on natural gas
Gulina S.A., Orlov M.Y., Mikheyenkov E.L.
Formation in the channels of the block catalyst the micro vortex gas flows with intense twist
Knysh Y.A., Zibizov Y.I., Dmitriev D.N., Gorshkalev A.A.
Studying the influence of the gas-dynamic non-stationary factors on the mathematical modelling of the gas turbine engines nonsetup work modes
Kofman V.M.
Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants
Matveev S.G., Abrashkin V.Y., Orlov M.Y., Lansky A.M., Makarov N.S., Matveev S.S., Anisimov M.Y.
Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation
Porter А.M., Bukatyi S.A., Leshin D.P.
Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure
Zrelov V.A., Makarchuk V.V., Prodanov M.E., Sudarev A.A.
Experimental investigation of turbulence of influence of the compressor’s out flow parameters on the hydraulics parameters resistance of separation diffuser of combustion chamber
Guryanova M.M.
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Investigation of the vibration behavior of a gas turbine engine in icing conditions
Danilkin S.Y., Teleshev V.A.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
About the probes for measuring pulsations of pressure in the flowing part gas turbine engines
Shorin V.P., Gimadiev A.G., Bystrov N.D., Ilinskij S.A.
Formation of microvortex gas flows in channels of a block catalyst with coplanar channels
Knysh Y.A., Tsibizov Y.I., Dmitriev D.N., Gorshkalev A.A.
Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator
Porter A.M., Bukaty S.A., Leshin D.P., Bukaty A.S.
Development of methods of modeling and computer aided design of gas turbine engines
Krivosheev I.A., Kozhinov D.G.
Gas turbine engine simulation strategy in CAE systems
Krivcov A.V.
Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure
1 1., 1 1., 1 1., 1 1.
Estimation of parameters of a pulse detonation engine (РDЕ)
Anakin A.T., Tsybizov Y.I.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Problems and solutions of using computer technologies in designing of combustion chambers GTE
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems
1 1., 1 1., 1 1., 1 1., 1 1.
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
Development of a neural network model of a micro gas turbine engine
Kuznetsov A.V., Makaryants G.M.
Hardening of blade gas turbine engines mixture balls and heated microballs
Krutsilo V.G.
The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method
Porter A.M., Bukatyi S.A., Leshin D.P., Vasilchuk M.V., Galickyi A.A.
the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш
1 1., 1 1., 1 1.
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time
Popov G.M., Baturin O.V., Novikova Y.D., Zubanov V.M., Volkov A.A., Korneeva A.I.
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems
Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.
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.
Selection of the design and application of plasma technology protective coatings parts gas turbine engines
Dokukina I.A.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel
Matveev S.G., Lanskiy A.M., Orlov M.Y., Abrashkin V.Y., Dmitriev D.N., Zubrilin I.A., Semenov A.V.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products
Boldyrev O.I., Gorynov I.M.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
1 - 39 of 39 Items

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