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Vol 18, No 3 (2019)

Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of computer modeling of the working process in small gas turbine engines

Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.

(Rus)

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

Gas turbine engine designing on the basis of a unified gas generator

Rybakov V.N.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

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.

(Rus)

Vol 18, No 2 (2019)

Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Approaches to modeling work of gas turbine engine`s core as a connected task

Krivcov A.V., Shabliy L.S., Baturin O.V.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Gas turbine engine simulation strategy in CAE systems

Krivcov 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 16, No 4 (2017)

Development of a new collector device for gas turbine engine afterburner

Teslya D.N., Mayatsky S.A., Grasko T.V.

(Rus)

Vol 19, No 4 (2020)

The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters

Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.

(Rus)

Vol 19, No 3 (2020)

Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger

Omar H., Kuz'michev V.S., Tkachenko A.Y.

(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)

1 - 13 of 13 Items

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