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Optimization of open counter – rotation fan blades on the basis of solving a 3D Navier-Stokes inverse problem with the aim of reducing tonal noise
Mileshin V.I., Rossikhin A.A., Pankov S.V., Shchipin S.K.
Fan engine research
Murzagaliev A.G., Nekrasov V.G.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Pyatunin K.R., Arkharova N.V.
Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads
Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.
Automated construction of a fan blade model according to data of CAD profile measurements
Arkhipov A.N., Bugrjashova E.V., Ravikovich Y.A., Savin R.A., Terentjev V.V., Shevjakov A.O.
Experimental design of a device for bird strike bench tests of non-rotating fan blades
Shorr B.F., Matsarenko V.S., Serebryakov N.N.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Numerical simulation of tonal noise of a bypass engine fan stage
Pyatunin K.R., Arharova N.V., Remizov A.E.
Reconstruction of fan blade dynamic loading prior to its fracture
Artamonov M.A., Govorov A.A., Starshinov D.S.
Computational investigation of aerodynamic and acoustic characteristics of an ultrahigh-bypass ratio counter-rotating fan
Druzhinin Y.M., Mileshin V.I., Rossikhin A.A.
The study of shrouded fan vibration modes and frequencies on holograph and as a part of the engine on the test rig
Koskin A.O., Seleznev V.G.
Improvement of fretting wear resistance of blade root made of polymer composite material
Karimbayev T.D., Afanasiev D.V., Matyukhin D.V., Orlov M.A.
Methods and the experiment of the parametric identification compressors and fans mathematical models of according to the results of the gas turbine engine development test
Kofman V.M.
Optimization of ducted counter–rotating fan blades on the basis of solving a 3d inverse problem with the aim of improving fan gasdynamic characteristics
Mileshin V.I., Pankov S.V., Fateyev V.A., Shchipin S.K.
GTE parts optimal design
Temis Y.M., Yakushev D.A.
Research of the fan blades flutter on the stalling airflow mode
Khorikov A.A., Danilkin S.Y.
Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques
Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.
1 - 19 of 19 Items

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