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Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket
Popov P.A., Sindyukov A.A., Kryuchkov A.N.
Calculating sound insulation of a sandwich structure on the basis of the «inverse matrix» method
Popov P.A., Osipov A.S., Sindyukov A.A.
Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
Shustov S.A.
Methodology of delivering space parts, tools and accessories to a near Earth orbital station on the basis of the reliability factor
Zheleznov I.V., Uperchuk R.A., Eroshenko V.K.
Ecological monitoring of megapolis on the basis of differential backscattering control of the wood culture
Zakharov V.P., Makurina O.N., Timchenko E.V., Timchenko P.E., Kotova S.P., Valliulov R.V.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Forecasting low-cycle fatigue life of gas-turbine engine parts by the method of equivalent tests for specimens with stress concentrator under extension-compression
Bukatyy S.A., Pakhomenkov A.V., Solntsev G.A., Bukatyy A.S.
Experimental research of the possibility of heat transfer enhancement in gas dynamic energy separation process
Popovich S.S., Vinogradov Y.A., Strongin M.M.
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.
Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
Modeling non-through surface cracks in the thin-walled structures
Skvortsov Y.V., Glushkov S.V.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
Processing of experimental data by the method of the least squares
Ovchinnikov A.V., Krasnochub E.K., Bronstein V.M.
Forces distribution in thread and external altering load factor in thread joint under structures vibration
Kurushin M.I., Kurushin A.M., Barmanov I.S.
Algorithm of monitoring the ecological state of coastal waters in areas of heavy economic use
Guryeva M.N., Zhuravel Y.N., Tishkin R.V.
Identification of scale factor of a pendulum compensating accelerometer during an orbital spacecraft mission
Fominov I.V.
Theoretical assessment of the influence of temperature on lattice spacing of aircraft gas-turbine engine turbine monocrystals
Badamshin I.K.
Reputation of enterprises competing in the market from the point of view of consumers
Ivanov D.Y., Kirilina Y.V.
Kinetic diagram of slow fatigue crack growth. Crack growth
Khibniсk T.A., Koltsoun Y.I.
Resonant converter with PWM output voltage adjustment
Vorokh D.A., Makhov A.I.
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
Popov P.A.
Design procedure of factor of rigidity of aviation elastic elements
Barmanov I.S.
Quality criteria hardened surface layer, the effective parameter management process technology of surface plastic deformation
Khibnidc T.A., Koltsoun Y.I.
Mathematical modeling of technological production process of thermo-stable resistor – capacity structures
Merkulov A.I., Laktanov P.V., Merkulov V.A.
The results of gas dynamic and strength improvement of turbocharger TK-32 axial turbine
Kolmakova D.A.
Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
Reconstruction of fan blade dynamic loading prior to its fracture
Artamonov M.A., Govorov A.A., Starshinov D.S.
About investigations the orientation dependence of single-crystal turbine blade exploitation properties
Tikhomirova E.A., Givushkin A.A., Sidokhin E.F.
Prospects of application of nanostructured heterophase polyfunctional composite materials in aero-engine manufacturing
Nizovtsev V.E., Klimov D.A., Bortnikov A.D., Nizovtsevа O.V.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
Processing of experimental data by the method of the least squares
1 1., 1 1., 1 1.
Analysis of the results of fatigue tests of cylindrical specimens with fillets using the method of finite element modeling
Vakulyuk V.S.
Isotopy of spacecraft compartment hull shapes
Belyakov A.A., Shulepov A.I.
The Laue back-reflection method for determination orientation and subgrains disorientation of blade manufacture single-crystal pieces
Tikhomirova E.A., Sidokhin E.F.
Research of the crack development process in a nickel heat-resistant alloyin the process of testing
Rozanov M.A.
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
Bolotov M.A., Zhidyaev A.N., Surkov O.S.
The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel
1 1., 1 1.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
Substantiation of the criteria for evaluation of the efficiency of the fuel supply system of the gas turbine engines
Smurova N.A.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities
Petrukhin A.G., Boev A.A., Butylkin S.V.
Calculation of the first resonant frequency and the first resonant factor of a sound absorption of material МR
1 1., 1 1., 1 1., 1 1.
1 - 43 of 43 Items

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