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Three-dimensional numerical investigations of the rotating detonation engine with a hollow combustor

机译:空心燃烧室旋转爆轰发动机的三维数值研究

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摘要

The aim of this work is to numerically verify a new model of the rotating detonation engine (RDE) combustor. The new model, which we call the hollow combustor, has no inner wall and is hollow. It is presented to solve the problem of engine heating that arises in RDEs with the co-axial annular combustor. Using the one-step chemistry kinetic model and the Euler equations in cylindrical coordinates, a series of three-dimensional (3D) numerical simulations are performed to find out whether detonation waves can propagate in such combustors. The results show that this new RDE combustor model can realize energy conversion in rotating detonation. The fuel-based specific impulse can reach around 7000 s. By comparing the results of hollow and annular combustors, some important differences are observed though general behaviors in these two RDE combustor models are similar. One is that there is no repeated reflection of shock waves in the hollow model. Another is that in the center of the cylinder part of fresh gas rolls inward into the region r < R-inner and here the RDE experiences some non-detonation burning. Also, through the comparison and analysis, roles of the outer and inner walls are presented. Without the restriction of the inner wall, burnt gas flows a little more divergently. (C) 2014 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:这项工作的目的是在数值上验证旋转爆轰发动机(RDE)燃烧器的新模型。我们称之为中空燃烧室的新模型没有内壁,而且是中空的。它被提出以解决在带有同轴环形燃烧器的RDE中出现的发动机加热问题。使用圆柱化学中的一步化学动力学模型和Euler方程,进行了一系列的三维(3D)数值模拟,以确定爆炸波是否可以在这种燃烧器中传播。结果表明,该新型RDE燃烧室模型可以实现旋转爆轰中的能量转换。基于燃料的比冲可达到约7000 s。通过比较中空和环形燃烧室的结果,尽管这两个RDE燃烧室模型的一般行为相似,但仍观察到一些重要差异。一个是空心模型中没有重复反射冲击波。另一个是,新鲜气体在气缸中心向内滚动到r

著录项

  • 来源
    《Combustion and Flame》 |2015年第4期|997-1008|共12页
  • 作者单位

    Peking Univ, State Key Lab Turbulence & Complex Syst, Dept Mech & Engn Sci, Ctr Combust & Prop, Beijing 100871, Peoples R China;

    Peking Univ, State Key Lab Turbulence & Complex Syst, Dept Mech & Engn Sci, Ctr Combust & Prop, Beijing 100871, Peoples R China;

    Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Rotating detonation; Hollow; Numerical simulation; Propulsion; Engine;

    机译:旋转爆轰;空心;数值模拟;推进;发动机;

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