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Authors
Investigation of extreme opportunities of stand supporting systems
Samsonov V.N., Kozyreva M.S., Cherevan A.A.
Features of dynamic processes in the “indentor – coating” system during tests on a tribometer
Kolesnikov I.V., Koropets P.A., Manturov D.S., Shakhmatov Y.V.
Dynamik experimental researches of the face gas dynamic seal
Novikov D.K., Balyakin V.B., Sedov V.V.
Special features of assessing the strength of nuclear reactor equipment under dynamic loads
Lonin K.A., Panov V.A., Patrushev V.L., Savchuk D.V., Soloviev S.A.
Imitation models of aircraft hydraulic units with account for typical faults
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Analysis of the influence of lubricant supply conditions on the pressure distribution in squeeze-film dampers
Novikov D.K., Shliandina N.S.
Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
Shustov S.A.
Use of phase portraits of hydro-mechanical units for diagnosing aircraft hydraulic systems
Gareyev A.M., Popelnyuk I.A.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
Numerical modeling on dynamic process of injection in supersonic part of the nozzle
Yakovchuk M.S.
Dynamic method of investigating stress concentrators of the YMZ-238 engine crankshaft considering surface hardening plastic deformation
Bukaty A.S., Kostichev V.E., Deniskina E.A.
Flight-navigation complex diagnostics at the aircraft manufacture stage
Koptev A.N., Kirillov A.V.
Mathematical modeling of the evolution of a tribosystem in the process of formation of equilibrium roughness of a frictional contact
Kolesnikov I.V., Koropets P.A., Manturov D.S., Shakhmatov Y.V.
The phenomenological models of the dynamic recrystallization of alloys for aviation
Khaimovich A.I., Surkov O.S.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
Early detection of vibration behaviour of aircraft engine multistage axial compressor in pre-surge states during rig testing
Khorikov A.A., Danilkin S.Y., Mazikina T.I.
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.
Investigation of structural damping of turbomashine blade vibrations using dynamic spin rigs
Nozhnitskiy Y.A., Fedina Y.A., Shadrin D.V.
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.
Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants
Vinogradov A.S.
Method of improving control using a simulation object model and its application to the problem of helicopter emergency landing manoeuvre optimization
Kvokov V.N., Trushkova Y.A., Ukhin M.Y.
Determination of loads on perforated tank partition
Filipov A.G., Glazkov I.E.
The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines
Kolesnikov A.S., Pakhol'chenko A.A.
Application of dynamic modeling to the evaluation of influence of strengthening treatment on fatigue resistance
Kostichev V.E.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
The influence of tether jamming on the motion of a space tether system during dynamic deployment
Ledkov A.S., Dyukov D.I.
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.
Dynamic loading and questions of assuring the reliability of functioning of superheavy launch vehicle cryogenic pressure-operated valves
Sazanov V.P.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
Calculating the dynamic error in measurement of electrohydromechanical system parameters, taking into account the operating speed of sensors
Gareyev A.M., Gimadiev A.G., Stadnik D.M., Popelnyuk I.A.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Dynamic of the a safety vent valve
Makaryjants M.V., Kudyurov L.V., Mustafaev Y.K., Tumanov D.V.
Shock wave profiles in relaxing gas with external energy source
Anchikov D.A., Galimov R.N., Zavershinskii D.I., Makaryan V.G., Molevich N.E.
A hot-wire anemometric transducer of airflow mass rate
Nikolayev V.N.
Modeling static and dynamic characteristics of pressure reducing valves
Igolkin A.A.
Research of dynamics of initiation, propagation, growth and closure of bubble cavities and a supercavity in a pipe with decontaminated liquid under hydraulic impacts
1 1.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion
Lobanov V.A.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
Van der Pol, Rayleigh and Duffing oscillators in discrete time dynamics
Zaitsev V.V., Nuraev D.B., Shilin A.N.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
Dynamic construction of the educational process in an integrated learning system
Grinberg G.M.
Stability of a rigid nonsymmetric rotor in elastic-damper sliding bearings
Ermilov Y.I.
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
Test rig for a hydraulic drive under switched inertance control
Shorin V.P., Sverbilov V.Y., Gimadiev A.G., Greshniakov P.I., Ilyukhin V.N., Stadnik D.M.
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.
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations
Ishkov S.A., Xiaoye X., Filippov G.A.
Dynamic elastic and damping models development and research for technical objects vibration safety providing
Shakirov F.M.
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.
Design and research of characteristics of a pressure fluctuation damping device for electrocontact manometers
Gimadiev A.G., Gimadiev A.A., Ermochkin A.Z., Ilyuchin V.N.
Dynamic positioning of a manned submersible over the service object
Alekseev A.V., Olenin A.L., Smirnov G.V., Fendrikov A.N.
Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure
1 1., 1 1., 1 1., 1 1.
Method of pipeline system designing taking into account complex interaction of static and dynamic processes with strength characteristics
Mironova T.B., Prokofiev A.B., Rodionov L.V.
Application of dynamic programming for path planning for observation of mobile ground targets in the controlled area
Lebedev G.N., Efimov A.V.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Application of stereolithography prototypes for gas dynamic tests
Matveev V.N., Shabliy L.S., Krivcov A.V.
Numerical solution of a production planning problem in case of dynamic labor input reduction
Pavlov O.V., Ryasnaya T.N.
Development of techniques and calculation program heterogeneous gas measurement circuits
Gimadiyev A.G., Bystrov N.D., Ustinov A.
Action of pulsed magnetic field on the melt in the manufacture of "metal-nonmetal" composites
Lazareva A.A.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Consideration of active forces at internal-combustion engine analysis in MSC.ADAMS environment
1 1., 1 1., 1 1.
Parametrical design of discrete mapping of Van der Pol oscillator
Zaitsev V.V., Nuraev D.B., Yudin A.N.
Some questions of designing and manufacture of wire material hub dampfers
Lazutkin G.V., Parovay F.V., Troynikov A.A.
Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine
Gimadiev A.G., Bystrov N.D., Dyagileva E.S.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Simulation design, kinematic and dynamic analysis of "virtual piston engine"
Gvozdev A.S., Melentjev V.S.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Fast algorithm for finding the resonance frequencies of gas turbine engine rotating blade disks
Davydov D.P.
Engine vibrations considering for light tugbocharger TKR-8,5C rotor journal bearing diagnostic
Ivanov D.Y., Filimonov M.K.
1 - 74 of 74 Items

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