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Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
Variations in free cross-sectional areas of the phases of double-phase flows under changes of gaseous phase rate of flow
Levkin Y.S.
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
Khramov A.A.
Test verification of flow stabilizer calculated parameters provided flow stabilization of propellant in wide range of input parameters
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example
Chicherova E.V.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov A.A.
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
Balakin V.L., Ishkov S.A., Khramov A.A.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
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.
Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines
Vasilyev A.J., Medvedev R.S., Chelebyan O.G.
Modeling oil separation in the impeller of a radial-type centrifugal breather
Petrukhin A.G., Tryanov A.E.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications
Grabovskiy A.A.
Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Guaranteeing of ecological and economic indicators of internal combustion engine
Grabovskiy A.A., Mironov V.A.
1 - 21 of 21 Items

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