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Vol 23, No 1 (2024)

Determination of completeness of combustion, temperature and emission characteristics in a swirl flow based on the theory of turbulent combustion

Aleksandrov Y.B., Mingazov B.G.

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

Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 15, No 4 (2016)

Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine

Semkin Y.V.

(Rus)

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

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.

(Rus)

Vol 10, No 5 (2011)

Modeling of fuel vaporization and mixing processes in combustion chamber

Tretiyakov V.V.

(Rus)

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

Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body

Didenko A.A., Sokolov A.B.

(Rus)

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

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

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

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.

(Rus)

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

Modeling of intrachamber processes in an oxygen-hydrogen thruster

Vaulin S.D., Salich V.L.

(Rus)

Vol 12, No 2 (2013)

Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components

Shustov S.A.

(Rus)

Vol 20, No 3 (2021)

Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine

Karev O.D.

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

Development of a generalized model of heat-mass transfer between fuel drops and gas stream with reference to gas turbine engine combustion chambers

Tretyakov V.V., Sviridenkov A.A.

(Rus)

Vol 20, No 3 (2021)

Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity

Aleksandrov Y.B., Nguyen T.D., Mingazov B.G.

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

Analyzing the quality of preparing fuel-air mixture and its influence on NOx in a low emission gas turbine engine combustion chamber

Markushin A.N., Baklanov A.V.

(Rus)

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

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

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

Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

1 - 20 of 20 Items

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