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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.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
Universal approach to the description of working medium chambers for simulating hydraulic and pneumatic systems
Timofeyev Y.M., Khalatov E.M.
Restarch tunetionality serewing tap by ultrasounl oscillation
Golovkin V.V., Trusov V.N.
Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications
Grabovskiy A.A.
Criteria for selecting categories of efficiency of soundproof materials used for car noise reduction
Fesina M.I., Krasnov A.V.
Guaranteeing of ecological and economic indicators of internal combustion engine
Grabovskiy A.A., Mironov V.A.
Converting sensor capacity into standardized signals with structural and time redundancy
Artamonov P.I.
Problematic issues of assessing the strength of axisymmetric parachute systems by conducting breakdown tests in flight experiments
Ivanov P.I., Kurinnyy S.M., Krivorotov M.M., Shmerova G.V.
Models for choosing admission campaign strategy of university in the contemporary context
Simanchuk N.V.
System approach to the choice of capacity of a high-speed radio data link for modern Earth remote sensing spacecraft
Kascheev A.A.
Approach to the assessment and forecasting for onboard computer systems of monitoring space vechiles during its usage based on full-scale experiments
1 1., 1 1., 1 1.
New possibilities of using spin rigs to provide gas turbine engine strength reliability
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V., Servetnik A.N., Baluev B.A., Kanachkin A.V., Lepeshkin A.R., Tomashev A.A., Chernyshev S.A.
Full-scale tests of superloaded thrust bearings for hydraulicturbine generators of Sibir hydroelectric power stations of the new generation with unit power of 1 million kw
Baiborodov Y.I.
Increasing the capacity of engine intake system
Kozin A.M., Rusakov M.M.
The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model
1 1., 1 1.
Using of heat-pipes with increased heat conduction as core elements of system of thermal control for aerospace equipment
, ,
1 - 18 of 18 Items

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