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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.
Comparison of quasi-three-dimensional and full three-dimensional formulations of thrust bearing operation
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body
Didenko A.A., Sokolov A.B.
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
Markushin A.N., Baklanov A.V.
Electrization of the surface of low-orbiting small spacecraft “AIST”
Syomkin N.D., Bragin V.V., Piyakov A.V., Telegin A.M., Ryazanov D.M., Matviets M.G.
Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process
Silyutin M.V.
Build-up mathematical model of allocation temperature gas along an axis the channel a torch discharge at interaction with thick-film devices of microassambly
Stolbikov A.V., Piganov M.N., Kostin A.V.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
Influence of tool deterioration on the density of heat flux distribution in the cutting area in end milling of OT4 titanium alloy
Evdokimov D.V., Skuratov D.L.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
The machine and methods of tribotehnical tests of materials
Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.
Thermophysical properties of multilayered structures
Rapilbekova N.S.
Choice of gas temperature at the turbopump turbine inlet
Ivanov A.V.
Formation of a model of rheological properties of hard-to-machine materials in the process of intensive cutting force deflection
Khaimovich A.I., Balaykin A.V., Galkina N.V.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
Calculation of cutting temperature at milling of purveyances from hard-processing materials
Trusov V.N., Skuratov D.L., Zakonov O.I., Shikin V.V.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Surging and auto-off the helicopter engine at start-up unguided missile from launchers
Prokopiev A.L., Povetkin O.V.
The concept of matching the joint operation of the combustion chamber, the compressor and the turbine
Grigoriev A.V., Golubchikov P.P., YIlushin M.Y., Rudakov O.A., Solovieva A.V.
Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block
Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Modeling thermal and thermomechanical effects in elements of microcircuits for the design of aircraft control airborne equipment
Fortinsky Y.K.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Research of influence the processes to afterhardening glass transition temperature of PKM
Postnov V.I., Burhan O.L., Rahmatullin A.E., Mantusova O.Y., Nikitin E.K.
Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state
Nikolayev V.N.
Relation between flame chemiionization and variable-volume combustion chamber temperature and pressure
Shaikin A.P., Galiev I.R.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
The equipment for research of properties of hydrocarbons at pressure from above 150 MPа
Rednikov S.N.
Criterial approach to constructing empirical models of cutting
Vinokurov M.V., Druzhin A.N.
On the efficiency of a radiant heating regenerative system
Panchenko V.V.
Experimental research of the possibility of heat transfer enhancement in gas dynamic energy separation process
Popovich S.S., Vinogradov Y.A., Strongin M.M.
Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio
Rybakov V.N.
Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine
Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.
1 - 36 of 36 Items

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