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首页|期刊导航|热科学学报(英文版)|3D Computation of Hydrogen-Fueled Combustion around Turbine Blade-Effect of Arrangement of Injector Holes -

3D Computation of Hydrogen-Fueled Combustion around Turbine Blade-Effect of Arrangement of Injector Holes -

Makoto YAMAMOTO Junichi IKEDA Kazuaki INABA

热科学学报(英文版)2006,Vol.15Issue(3):233-239,7.
热科学学报(英文版)2006,Vol.15Issue(3):233-239,7.

3D Computation of Hydrogen-Fueled Combustion around Turbine Blade-Effect of Arrangement of Injector Holes -

3D Computation of Hydrogen-Fueled Combustion around Turbine Blade-Effect of Arrangement of Injector Holes -

Makoto YAMAMOTO 1Junichi IKEDA 2Kazuaki INABA1

作者信息

  • 1. Department of Mechanical Engineering, Tokyo University of Science 1-3 Kagurazaka, Shinjuku-ku,Tokyo, 162-8601, Japan
  • 2. Graduate School of Mechanical Engineering, Tokyo University of Science 1-3 Kagurazaka, Shinjuku-ku,Tokyo, 162-8601, Japan
  • 折叠

摘要

Abstract

Recently, a number of environmental problems caused from fossil fuel combustion have been focused on. In addition, with the eventual depletion of fossil energy resources, hydrogen gas is expected to be an alternative energy resource in the near future. It is characterized by high energy per unit weight, high reaction rate, wide range of flammability and the low emission property. On the other hand, many researches have been underway in several countries to improve a propulsion system for an advanced aircraft. The system is required to have higher power, lighter weight and lower emissions than existing ones. In such a future propulsion system, hydrogen gas would be one of the promising fuels for realizing the requirements. Considering these backgrounds, our group has proposed a new cycle concept for hydrogen-fueled aircraft propulsion system. In the present study, we perform 3dimensional computations of turbulent flow fields with hydrogen-fueled combustion around a turbine blade. The main objective is to clarify the influence of arrangement of hydrogen injector holes. Changing the chordwise and spanwise spacings of the holes, the 3 dimensional nature of the flow and thermal fields is numerically studied.

关键词

computational fluid dynamics/turbine blade/hydrogen combustion/injector hole arrangement

Key words

computational fluid dynamics/turbine blade/hydrogen combustion/injector hole arrangement

分类

航空航天

引用本文复制引用

Makoto YAMAMOTO,Junichi IKEDA,Kazuaki INABA..3D Computation of Hydrogen-Fueled Combustion around Turbine Blade-Effect of Arrangement of Injector Holes -[J].热科学学报(英文版),2006,15(3):233-239,7.

热科学学报(英文版)

OAEISCI

1003-2169

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