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Vol 22, No 3 (2023)

Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine

Belonozhkin V.V., Teslya D.N.

(Rus)

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

Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection

Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.

(Rus)

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

Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example

Chicherova E.V.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 17, No 2 (2018)

Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 11, No 1 (2012)

Command control of hypersonic cruising aircraft during climb

Balakin V.L., Kotchyan A.G.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

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

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

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

Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications

Grabovskiy A.A.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand

Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.

(Rus)

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

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 18, No 1 (2019)

Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle

Khramov A.A.

(Rus)

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

Test verification of flow stabilizer calculated parameters provided flow stabilization of propellant in wide range of input parameters

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

1 - 13 of 13 Items

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