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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.
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.
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
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.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
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.
Joint works of Ilyushin design bureau and general designer N. D. Kuznetsov
Novozhilov G.V.
Analysis of the influence of lubricant supply conditions on the pressure distribution in squeeze-film dampers
Novikov D.K., Shliandina N.S.
Empirical metod of predicting aviation piston engine noise
Moshkov P.A.
Improving the quality parameters of serial debug two spool mixed flow turbofan
Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.
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.
Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer
Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.
1
1 1., 1 1.
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.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Noise reduction of snow-plough
1 1., 1 1., 1 1., 1 1.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
Feature of optimization of parameters of working process GTE with the free turbine at initial designing in the conditions of uncertainty
1 1., 1 1.
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.
Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks
Kutyrev V.V., Teplova S.V.
1 - 24 of 24 Items

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