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Authors

Vol 10, No 3-3 (2011): Special Issue

Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 22, No 1 (2023)

The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)

Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.

(Rus)

Vol 23, No 2 (2024)

Comparative results of computational and theoretical study of the annular nozzle with a flat central body

Kirshina A.A., Levikhin A.A., Kirshin A.Y.

(Rus)

Vol 23, No 2 (2024)

Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles

Ageenko Y.I., Bubnova A.S.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

Vol 21, No 2 (2022)

Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing

Parovay E.F.

(Rus)

Vol 21, No 2 (2022)

3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes

Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.

(Rus)

Vol 8, No 1 (2009)

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.

(Rus)

Vol 19, No 4 (2020)

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.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

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.

(Rus)

Vol 9, No 1 (2010)

Dynamic analysis and optimization of turbojet engine nozzle control mechanism

(Rus)

Vol 7, No 3 (2008): Special Issue

Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage

Baturin O.V., Matveev V.N.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

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.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

Vol 12, No 2 (2013)

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.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

The analysis of real thermodynamic cycle of bypass engine with mixing

Medvedev V.V.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

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.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics

Matveev S.G., Orlov M.Y., Zubrilin I.A.

(Rus)

Vol 16, No 2 (2017)

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.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber

Vasilyev A.J., Blumkin P.I., Chelebyan O.G.

(Rus)

Vol 15, No 4 (2016)

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.V.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Effect of coagulation of drops on fuel spray characteristics behind atomizers

1 1., 1 1.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system

Veretennikov S.V., Khasanov S.M.

(Rus)

Vol 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.A.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

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.

(Rus)

Vol 13, No 1 (2014)

Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets

Ivanov I., Kryukov I., Shustov S.

(Rus)

Vol 8, No 1 (2009)

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.

(Rus)

Vol 20, No 4 (2021)

Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics

Tishchenko K.O., Brykov N.A., Belyaeva A.S.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Development of the construction of a gas turbine engine vane with built-in vortex tubes

Veretennikov S.V., Barinov S.N.

(Rus)

Vol 9, No 2 (2010): Special Issue

Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent

1 1., 1 1., 1 1., 1 1.

(Rus)

1 - 33 of 33 Items

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