ISSN 2079-3537      

 
 
 
                                                                                                                                                                                                                                                                                                                                                                                                                                                                             
Scientific Visualization
Issue Year: 2011
Quarter: 2
Volume: 3
Number: 2
Pages: 54 - 63
Article Name: VISUALIZATION DURING DEVELOPING OF THE FINISHING MILLING PROCESS OF THE COMPRESSOR BLADE'S AERODYNAMIC MODEL FROM GAS TURBINE ENGINE (GTE) WITH OPEN ROTOR
Authors: S. Bolsunovskiy (Russia), V. Vermel (Russia), G. Gubanov (Russia), I. Kacharava (Russia).
Address: S. Bolsunovskiy
sa_bolsunovskiy@mail.ru
Central Aerohydrodynamics Institute "TsAGI”, Zhukovskiy, Russia
 
V.Vermal
vermel@tsagi.ru
Central Aerohydrodynamics Institute "TsAGI”, Zhukovskiy, Russia
 
G. Gubanov
glebgubanov@mail.ru
Central Aerohydrodynamics Institute "TsAGI”, Zhukovskiy, Russia
 
I. Kacharava
Iraklykacharava@rambler.ru
Central Aerohydrodynamics Institute "TsAGI”, Zhukovskiy, Russia
Abstract: We describe the results of scientific work carried out from 2008 to 2010 in Central Aero-Hydrodynamic Institute (TsAGI). This work is focused on developing high-speed milling technology of thin-walled parts, such as rotor blades of gas turbine engine (GTE), within the framework of European cooperative project DREAM. In particular, we consider unconventional treatment process of aerodynamic model of compressor blade from GTE with open rotor. The results demonstrate convincingly efficiency of using software tools with visualization capabilities of research activity.
Language: Russian