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Title
Authors
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200
Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.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.
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Ageenko Y.I., Ilyin R.V., Pegin I.V.
Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage
Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
Vasilyev A.J., Blumkin P.I., Chelebyan O.G.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
Markushin A.N., Baklanov A.V.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
Development of the construction of a gas turbine engine vane with built-in vortex tubes
Veretennikov S.V., Barinov S.N.
Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow
Teslya D.N., Mityaev S.V., Drobyshev P.A.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip
Shustov S.A.
Numerical modeling and experimental research of a two-phase liquid- gas ejector with a profiled supersonic nozzle
Lepeshinsky I.A., Reshetnikov V.A., Zarankevich I.A.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
Engineering design and experimental research of non-metallic parts and components of the hot section of the advanced gas turbine engine
Karimbayev T.D., Mezentsev M.A., Ezhov A.J.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Mathematical modelling and parametric research of flow of the twisted turbulent single-component stream of the propulsive mass in the trance- and supersonic areas of Laval nozzles
1 1., 1 1.
Effect of coagulation of drops on fuel spray characteristics behind atomizers
1 1., 1 1.
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Dynamic analysis and optimization of turbojet engine nozzle control mechanism
Experimental development of the LRE with CCCM nozzle’s extension
,
1 - 27 of 27 Items

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