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The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade
Matveev V.N., Melnikov S.A., Popov G.M., Zubanov V.M., Kudryashov I.A., Shcherban A.I.
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience
Alendar A.D., Grunin A.N., Siluyanova M.V.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.A.
Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system
Sychev A.V., Arbuzov I.V., Ravikovich Y.A.
Aircraft electric power plants
Kondryakov A.D., Leontiev M.K.
The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry
Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Empirical metod of predicting aviation piston engine noise
Moshkov P.A.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
Joint works of Ilyushin design bureau and general designer N. D. Kuznetsov
Novozhilov G.V.
Some issues of research and development in aviation industry
Korchak V.Y., Kuznetsov V.V., Borisenkov I.L., Leonovich G.I., Lukachev S.V., Biryuk V.V.
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.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Improving the quality parameters of serial debug two spool mixed flow turbofan
Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.
Aspects of simulating stable low-cycle fatigue crack growth in the main parts of aircraft gas turbine engines
Ryabov A.A., Mokhov K.Y., Voronkov O.V., Kudryavtsev A.Y., Museev A.A.
Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic
Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
Construction of a promising face gas-dynamic seal of the aircraft engine
Bondarchuk P.V., Falaleev S.V.
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.A.
Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics
Kustov O.Y., Khramtsov I.V., Bulbovich R.V.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Analysis of economic and organizational problems in aircraft engine construction
Nikitin N.F., Cherner N.V.
The phase characteristic of force cutting and its role in occurrence and development of self-oscillations at sharpening not rigid details of aviation engines
Burmistrov E.V., Basyrov M.N., GiniyatuIIin R.R.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
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