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Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor

机译：当来自液体冷却涡轮机的热量在主压缩机之前，之内或之后被排除时，燃气涡轮机发动机性能

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Esgar, Jack B; Slone, Henry O;
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年度 1956
页码 1-41
总页数 41
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Gas turbine exhaust-gas heat utilization of main gas pipeline gas-compressor units [J] . REDKO A.O., REDKO O.F., KOMPAN A.I. Нафтова и газова промысловисть . 2013,第4期

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2. Miniature gas turbines: Numerical study of the effects of heat transfer and Reynolds number on the performance of an axial compressor [J] . Junting Xiang, Joerg Uwe Schlueter, Fei Duan International Journal of Computational Materials Science and Engineering . 2014,第2期

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3. Thermodynamic performance assessment of an indirect intercooled reheat regenerative gas turbine cycle with inlet air cooling and evaporative aftercooling of the compressor discharge [J] . A. Khaliq, K. Choudhary International journal of energy research . 2006,第15期

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5. Off-Design Performance Prediction of Gas Turbines without the use of Compressor or Turbine Characteristics. [D] . Suraweera, Janitha Kanishka. 2012

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Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor

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