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Authors
Development and analysis of models of heat transfer in compact porous heat exchangers of aero space control systems
Konovalov D.A.
A hot-wire anemometric transducer of airflow mass rate
Nikolayev V.N.
Modeling of the heat exchange processes
Limanova N.I., Mamzin E.A., Matveev S.G.
On the efficiency of a radiant heating regenerative system
Panchenko V.V.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Experimental research of internal heat transfer in the vortex heat generator
Zhornik M.N., Piralishvili S.A., Mogileva K.A.
Vortex effect and intensification of heat and mass transfer in cell energy technology
Piralishvily S.A., Veretennikov S.V.
Thermophysical properties of multilayered structures
Rapilbekova N.S.
Experimental investigation of heat transfer in energy separation chambers of the vortex tube
Veretennikov S.V., Barinov S.N.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Development of a generalized model of heat-mass transfer between fuel drops and gas stream with reference to gas turbine engine combustion chambers
Tretyakov V.V., Sviridenkov A.A.
Numerical simulation of heat transfer from a swirling flow to the lateral side of the vortex tube energy separation chamber
Piralishvili S.A., Sokolova A.A.
Physical principles of hydrodynamic non-stationarity effect on turbulent flow
Krayev V.M., Tikhonov A.I.
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.
Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod
1 1., 1 1., 1 1.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
Experimental research of heat exchange in a plane channel using the regular thermal regime mrthod with different Biot numbers
Kolesova E.G., Veretennikov S.V., Zhornik M.N.
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.
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.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
1 - 22 of 22 Items

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