Development of Effective Cooling Schemes of Gas Turbine Blades Based on Computer Simulation

被引：0
|
作者：
Pasayev, A. [1 ]
Askerov, C. [1 ]
Sadiqov, R. [1 ]
Ardil, C. [1 ]
机构：
[1] Azerbaijan Natl Acad Aviat, Baku 370057, Azerbaijan
来源：
PROCEEDINGS OF WORLD ACADEMY OF SCIENCE, ENGINEERING AND TECHNOLOGY, VOL 23 | 2007年 / 23卷
关键词：
multi coherent systems; method of the boundary integrated equations; singular operators; gas turbines;
D O I：
暂无
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
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.
引用
收藏
页码：523 / 528
页数：6
相关论文
共 50 条
  • [41] INVESTIGATION OF HYDRAULIC RESISTANCE OF COOLING PATH OF GAS TURBINE FIXED BLADES
    SHUVALOV, GI
    MARIEV, DI
    BALASHOV, YA
    THERMAL ENGINEERING, 1969, 16 (09) : 78 - &
  • [42] A numerical procedure to design internal cooling of gas turbine stator blades
    Carcasci, C
    Facchini, B
    REVUE GENERALE DE THERMIQUE, 1996, 35 (412): : 257 - 268
  • [43] FILM COOLING MODELLING FOR GAS TURBINE NOZZLES AND BLADES: VALIDATION AND APPLICATION
    Andrei, Luca
    Innocenti, Luca
    Andreini, Antonio
    Facchini, Bruno
    Winchler, Lorenzo
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 5B, 2015,
  • [44] Application of iterative algorithms for gas-turbine blades cooling optimization
    Frackowiale, Andrzej
    Cialkowski, Michal
    Wroblewska, Agnieszka
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2017, 118 : 198 - 206
  • [45] Recent Advances in Cooling Technology for the Leading Edge of Gas Turbine Blades
    Zhu, Shixing
    Li, Yan
    Yan, Junyang
    Zhang, Chao
    ENERGIES, 2025, 18 (03)
  • [46] Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance
    Agata, Yukiko
    Takahashi, Toshihiko
    Sakai, Eiji
    Nishino, Koichi
    JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2012, 7 (04): : 603 - 618
  • [47] A review of recent studies on rotating internal cooling for gas turbine blades
    Yeranee, Kirttayoth
    Rao, Yu
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (07) : 85 - 113
  • [48] COMPUTER SIMULATION OF FATIGUE, CREEP AND THERMAL-FATIGUE CRACKS PROPAGATION IN GAS-TURBINE BLADES
    Semenov, Artem
    Semenov, Sergey
    Nazarenko, Anatoly
    Getsov, Leonid
    MATERIALI IN TEHNOLOGIJE, 2012, 46 (03): : 197 - 203
  • [49] Effect of Cooling Parameters on the Thermostressed State of Gas Turbine Nozzle Blades
    Karpinos, B. S.
    Kulish, V. M.
    STRENGTH OF MATERIALS, 2017, 49 (03) : 412 - 421
  • [50] STUDY OF PARTICLES DEPOSITION IN GAS TURBINE BLADES IN PRESENCE OF FILM COOLING
    Borello, Domenico
    D'Angeli, Luca
    Salvagni, Alessandro
    Venturini, Paolo
    Rispoli, Franco
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5B, 2014,
12345