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Title
Authors
Interaction of exhaust jets of rocker propulsions on various propellants with atmosphere for estimation of ecological safety of firing of rockets and launchers
Zavelevich F.S., Ushakov N.N.
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.
Method for determining the energy of jets vibration waves
Limanova N.I., Levkin Y.S.
Numerical modeling on dynamic process of injection in supersonic part of the nozzle
Yakovchuk M.S.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov A.A.
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.
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Gas-discharge generation of near-wall flows
Ivchenko A.V., Zhuravliov O.A., Shakhov V.G.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Thermodynamic shape of the combined power installations, based on GTU and solid oxide fuel cells
Loskutnikov A.A., Gorjunov I.M., Bakirov F.G.
Experimental study of swirled gas flow by the particle image velocimetry method
Knysh Y.A., Redkin Y.S., Dmitriev D.N.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession
Sviridenkov A.A., Tretyakov V.V.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Experimental study of free-convection flame propagation
Yevdokimov O.A., Guryanov A.I.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
Manipulate pulsed detonation engine
1 1., 1 1.
1 - 19 of 19 Items

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