首页> 美国政府科技报告 >EFFECTS OF FUEL-NOZZLE CARBON DEPOSITION ON COMBUSTION EFFICIENCY OF SINGLE TUBULAR-TYPE, REVERSE-FLOW TURBOJET COMBUSTOR AT SIMULATED ALTITUDE CONDITIONS
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EFFECTS OF FUEL-NOZZLE CARBON DEPOSITION ON COMBUSTION EFFICIENCY OF SINGLE TUBULAR-TYPE, REVERSE-FLOW TURBOJET COMBUSTOR AT SIMULATED ALTITUDE CONDITIONS

机译:燃料 - 喷嘴碳沉积对模拟高原条件下单管式逆流涡轮喷射燃烧器燃烧效率的影响

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摘要

An investigation was conducted in order to study the effects of changes in fuel-nozzle carbon deposition on the combustion efficiency of a single tubular-type, reverse-flow, turbojet combustor. This investigation was conducted because of the need to improve the reproducibility of combustion data for fuel-research purposes. The inlet-air conditions simulated operation of a single tubular-type combustor of a turbojet engine in the range of altitudes from 20,000 to 45,000 feet and the range of engine speeds from 10,000 to 15,000 rpm.

著录项

  • 作者

    Ralph T. Dittrich;

  • 作者单位
  • 年度 1948
  • 页码 1-29
  • 总页数 29
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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