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Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade
Matveev V.N., Melnikov S.A., Popov G.M., Zubanov V.M., Kudryashov I.A., Shcherban A.I.
3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes
Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.
Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage
Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.
Mathematical modeling of heat exchange on air cooling of a number of aluminum ingots
Gorshenin A.S.
Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor
Panchenko S.L., Gras’ko T.V.
Agreement between criterial equations of heat transfer in the process of cooling aluminium ingots and experimental data
Gorshenin A.S., Krivosheev V.E.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Increasing the efficiency of rotary piston engines by the use of the diesel cycle
Okorochkov V.V., Okorochkova V.M., Ravodin A.I.
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling
Vorobiev A.G., Borovik I.N., Ha S.
Thermal state of a groind-use gas turbine engine stator
Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.
Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples
Lebedev V.V., Lebedev O.V., Remizov A.E.
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods
Matveev S.G., Anisimov V.M., Zubrilin I.A., Kolomzarov O.V., Mironov N.S.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems
1 1., 1 1.
Issues of evolution of rotor piston engines’ subject abroad and in Russia
Kocherov E.P., Kononov V.A., Okorochkov V.V., Okorochkova V.M., Ivanova K.P.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Numerical investigation of phisical processes in cooling jacket of thrust chamber of LOx – LH2 LRE using 3D computer simulation methods
Yakub P.A., Gumennyy A.V.
Selection of new heat-resistant nickel alloys for advanced aviation engines
1 1., 1 1., 1 1., 1 1., 1 1.
Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
Mathematical modeling and investigation of the process of thermal theatment of aluminum ingots on the basis of regulated convective heat transfer
Gorshenin A.S., Krivosheev V.E.
The analyze of work of throttle cooling system’s microheat exchanger, wich uses nitrogen with nearly critical parameters
1 1., 1 1., 1 1., 1 1.
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium
Sokolov M.A., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Tkachenko A.Y.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
3d calculation of a multiport low-emission combustor cooling system
Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.
Particularity of thermal condition computation oF LRE with cooling by liquid oxygen
1 1.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
Thermal state of combustor can elements
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
Heat-pipes’ application for cooling of communications-electronics equipment
Biryuk V.V., Kitaev A.I.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Automated selection of cooling system for radio electronic design of thermophysical
Goryachev N.V., Trusov V.A., Yurkov N.K.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.
Increase in thermal efficiency of the conditioned clothing
Savchenko N.V.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system
Dovgjallo A.I., Sarmin D.V., Uglanov D.A.
1 - 37 of 37 Items

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