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Gas dynamic optimization of the work process of a single-stage cooled axial turbine with an inside baffle
Popov G.M., Goryachkin E.S., Melnikov S.A., Shcherban A.I., Gataullina E.D.
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.
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Approaches to modeling work of gas turbine engine`s core as a connected task
Krivcov A.V., Shabliy L.S., Baturin O.V.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Methods of modeling the work process of hydrogen screw-centrifugal pumps using ANSYS CFD
Sulinov A.V., Shabliy L.S., Zubanov V.M.
Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants
Nigodjuk V.E., Sulinov A.V.
Gas turbine engine simulation strategy in CAE systems
Krivcov A.V.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
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