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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.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
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.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.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.
Thermal state of a groind-use gas turbine engine stator
Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.
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.
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.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
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.
3d calculation of a multiport low-emission combustor cooling system
Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.
1 - 14 of 14 Items

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