Heat transfer in the blading of a gas turbine engine

被引：0
|
作者：
Dorfman, A.Sh. [1 ]
Davydenko, B.V. [1 ]
机构：
[1] Engineering Heat-Physics Inst, Russia
来源：
Thermal Engineering (English translation of Teploenergetika) | 1988年 / 35卷 / 11期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
2
引用
收藏
页码：627 / 630
相关论文
共 50 条
  • [21] COUPLED SIMULATION OF THE SECONDARY AIR FLOW, HEAT TRANSFER, AND STRUCTURAL DEFLECTION OF A GAS TURBINE ENGINE
    Tondello, Guilherme
    Boruszewski, Wolodymir
    Menge, Fernando
    Assato, Marcelo
    Shimizu, Silvio
    Ziegler, Shayne
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 2295 - +
  • [22] Methods for coupled fluid/solid heat transfer with application on aircraft engine gas turbine components
    Negulescu, D.A.
    Berbente, C.
    UPB Scientific Bulletin, Series D: Mechanical Engineering, 2002, 64 (04): : 81 - 99
  • [23] Derivation of signatures for faults in gas turbine compressor blading
    Aretakis, N
    Mathioudakis, K
    Dedoussis, V
    (SAFEPROCESS'97): FAULT DETECTION, SUPERVISION AND SAFETY FOR TECHNICAL PROCESSES 1997, VOLS 1-3, 1998, : 79 - 84
  • [24] EFFECTS OF FREE-STREAM TURBULENCE INTENSITY AND FREQUENCY ON HEAT-TRANSFER TO TURBINE BLADING
    BAYLEY, FJ
    PRIDDY, WJ
    JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1981, 103 (01): : 60 - 64
  • [25] NEW NICKEL ALLOY FOR GAS TURBINE BLADING.
    Just, Ch.
    Sulzer Technical Review, 1980, 62 (01): : 27 - 29
  • [26] Derivation of signatures for faults in gas turbine compressor blading
    Aretakis, N
    Mathioudakis, K
    Dedoussis, V
    CONTROL ENGINEERING PRACTICE, 1998, 6 (08) : 969 - 974
  • [27] Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine
    Arunkumar, G. L.
    Shetty, Balachandra P.
    Mishra, R. K.
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2023, 40 (01) : 93 - 100
  • [28] Effects of a pocket cavity on heat transfer and flow characteristics of the endwall with a bluff body in a gas turbine engine
    Liu, Jian
    Hussain, Safeer
    Wang, Lei
    Xie, Gongnan
    Sunden, Bengt
    APPLIED THERMAL ENGINEERING, 2018, 143 : 935 - 946
  • [29] The Effect of Heat Transfer Coefficient Increase on Tip Clearance Control in HP Compressors in Gas Turbine Engine
    Ekong, Godwin Ita
    Long, Christopher A.
    Childs, Peter R. N.
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2013, VOL 1, 2014,
  • [30] Heat transfer in translucent thermal barrier coatings of turbine engine
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2000, 15 (03): : 268 - 273
12345