THE ROLE OF LAMINAR-TURBULENT TRANSITION IN GAS-TURBINE ENGINES

被引:693
作者
MAYLE, RE
ROBERTS, WB
机构
[1] RENSSELAER POLYTECH INST, TROY, NY 12180 USA
[2] FLOW APPLICAT RES, FREMONT, CA 94539 USA
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1991年 / 113卷 / 04期
关键词
D O I
10.1115/1.2929110
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A critical study of laminar-turbulent transition phenomena and their role in aerodynamics and heat transfer in modern and future gas turbine engines is presented. In order to develop a coherent view of the subject, a current look at transition phenomena from both a theoretical and experimental standpoint are provided and a comprehensive state-of-the-art account of transitional phenomena in the engine's throughflow components given. The impact of transitional flow on engine design is discussed and suggestions for future research and developmental work provided.
引用
收藏
页码:509 / 537
页数:29
相关论文
共 111 条
  • [81] PAXSON DE, 1989, THESIS RENSSELAER PO
  • [82] PFEIL H, 1979, ASME79GT128 PAP
  • [83] PFEIL H, 1983, ASME T, V105, P130
  • [84] RILEY S, 1989, ASME89GT321 PAP
  • [85] CALCULATION OF LAMINAR SEPARATION-BUBBLES AND THEIR EFFECT ON AIRFOIL PERFORMANCE
    ROBERTS, WB
    [J]. AIAA JOURNAL, 1980, 18 (01) : 25 - 31
  • [86] RUD K, 1986, ASME, V108, P116
  • [87] SCHLICHTING H, 1991, ASME, V113, P10
  • [88] Schlichting H., 1979, BOUNDARY LAYER THEOR
  • [89] SCHRAUB FA, 1965, MD12 STANF U MECH EN
  • [90] SCHRODER T, 1989, 1989 EUR PROP FOR BA, V15, P1