Development of Effective Cooling Schemes of Gas Turbine Blades Based on Computer Simulation
In contrast to existing of calculation of temperature field of a profile part a blade with convective cooling which are not taking into account multi connective in a broad sense of this term, we develop mathematical models and highly effective combination (BIEM AND FDM) numerical methods from the point of view of a realization on the PC. The theoretical substantiation of these methods is proved by the appropriate theorems.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1058855Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1225
 Pashaev A.M., Sadykhov R.A., Iskenderov M.G., Samedov A.S., Sadykhov A.H. (1997). The effeciency of potential theory method for solving of the tasks of aircraft and rocket design. 10-th National Mechanic Conference. Istanbul Technical University, Aeronautics and astronautics faculty, Istanbul, Turkey, July, p.61-62. 1997.
 R.A. Sadigov, A.S. Samedov, (1998). Modelling of temperature fields of elements of base turbines, scientists of a slip ¶Çê║zTU, Baku, Vol.VI, ¶Çèï 5, p.234-239.
 Pashaev A.M., Sadykhov R.A., Samedov A.S. (1999). Highly effective methods of calculation temperature fields of blades of gas turbines. V International Symposium an Aeronautical Sciences "New Aviation Technologies of the XXI century", A collection of technical papers, section N3, Zhukovsky, Russia, August 1999.
 L.N. Zisina-Mologen and etc., (1974). Heat Exchange in turbineengines. M.,
 G. Galicheiskiy, (1996). A thermal guard of blades, ¶Çëå.: ¶Çëå¶Çê║I, 1996.
 A.M.Pashaev, R.A.Sadiqov, C.M.Hajiev, (2002). The BEM Application in development of Effective Cooling Schemes of Gas Turbine Blades. 6th Bienial Conference on Engineering Systems Design and Analysis, Istanbul, Turkey, July, 8-11.