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Vol 62, No 3 (2019)

3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes

Gorelov Y.G.

(Eng)

Vol 60, No 3 (2017)

The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft

Ermakov S.A., Lalabekov V.I., Samsonovich S.L.

(Eng)

Vol 62, No 2 (2019)

Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint

Konstantinov S.V., Lalabekov V.I., Obolenskii Y.G.

(Eng)

Vol 60, No 2 (2017)

Thermal state of the shell for supersonic part of the ramjet nozzle

Zarubin G.P., Zimin V.N., Kuvyrkin G.N.

(Eng)

Vol 61, No 4 (2018)

Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles

Krioukov V.G., Abdullin A.L., Nikandrova M.V., Safiullin I.I.

(Eng)

Vol 60, No 1 (2017)

Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles

Kryukov V.G., Abdullin A.L., Demin A.V.

(Eng)

Vol 61, No 2 (2018)

Peculiarities of Mixture Formation and Ignition of the Fuel Mixture in the Metal Sprayer Chamber

Ryazanov A.I., Egorychev V.S.

(Eng)

Vol 60, No 1 (2017)

A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber

Baklanov A.V., Neumoin S.P.

(Eng)

Vol 61, No 2 (2018)

Simulation of a Rocket Engine Nozzle Discharge Coefficient

Sabirzyanov A.N., Glazunov A.I., Kirillova A.N., Titov K.S.

(Eng)

Vol 59, No 4 (2016)

A method of design calculation for the two-component jet-jet gas nozzle with outer mixing

Egorychev V.S., Ryazanov A.I.

(Eng)

Vol 61, No 1 (2018)

Gas and Powder Flow Optimization in a Four-Jet Laser Cladding Head

Shpilev A.I., Iskhakov F.R., Nagulin K.Y., Gil’mutdinov A.K.

(Eng)

Vol 59, No 4 (2016)

Thermal radiation of heterogeneous combustion products at the nozzle exit of the rocket microengine

Kuz’min V.A., Maratkanova E.I., Zagrai I.A., Rukavishnikova R.V.

(Eng)

Vol 61, No 1 (2018)

The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes

Gorelov Y.G., Tyul’kov K.V.

(Eng)

Vol 60, No 4 (2017)

Numerical Research of Intra-Chamber Processes Dynamics during Startup of a Special Solid Propellant Engine

Egorov M.Y.

(Eng)

1 - 14 of 14 Items

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