首页> 外文期刊>International journal of hydrogen energy >Recent advances in cavity-based scramjet engine- a brief review
【24h】

Recent advances in cavity-based scramjet engine- a brief review

机译:基于腔的超燃冲压发动机的最新进展-简要回顾

获取原文
获取原文并翻译 | 示例
       

摘要

At present, the critical issue related to design of scramjet engine is to achieve efficient mixing between the air and fuel. Among the several fuel injection strategies, cavity flame holder is identified as a well-organized method for supporting the ignition zone. In this review, some mixing enhancement approaches based on well-known cavity based injection scheme proposed in latest research works, are summarized in detailed. The influence of cavity on the performance of scramjet combustor is recapitulated from three aspects, namely variation of shape/geometry of cavity flame holder; location of fuel/air injection scheme; and recent progresses in dual/double cavity. This review reveals that the cavity rear wall-expansion is an innovative kind of cavity flame holder which has a great impact on the efficiency of scramjet combustor whereas the presence of micro air jets have improved the flame holding mechanism of scramjet engine. Additionally, the performance of scramjet is significantly improved by dual cavity indicating that the dual cavity flame holder would be a feasible preference for the future growth of scramjet engine. (C) 2019 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
机译:当前,与超燃冲压发动机的设计有关的关键问题是实现空气和燃料之间的有效混合。在几种燃料喷射策略中,腔火焰保持器被认为是组织良好的支撑点火区的方法。在这篇综述中,详细总结了最新研究工作中提出的基于众所周知的基于腔的注射方案的混合增强方法。从三个方面概括了腔室对超燃喷射燃烧器性能的影响,即腔室火焰保持器的形状/几何形状的变化;燃油/空气喷射方案的位置;和双腔/双腔的最新进展。这篇评论揭示了腔体后壁的膨胀是一种创新的腔体火焰保持器,它对超燃冲压燃烧器的效率有很大的影响,而微型喷气的存在改善了超燃冲压发动机的火焰保持机制。此外,双腔显着改善了超燃冲压发动机的性能,表明双腔火焰保持器将是超燃冲压发动机未来发展的可行选择。 (C)2019氢能出版物有限公司。由Elsevier Ltd.出版。保留所有权利。

著录项

  • 来源
    《International journal of hydrogen energy》 |2019年第26期|13895-13909|共15页
  • 作者单位

    MITS UGC Autonomous Inst, Dept Mech Engn, Madanapalle 517325, Andhra Pradesh, India;

    MITS UGC Autonomous Inst, Dept Mech Engn, Madanapalle 517325, Andhra Pradesh, India;

    Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China;

    MITS UGC Autonomous Inst, Dept Mech Engn, Madanapalle 517325, Andhra Pradesh, India;

    MITS UGC Autonomous Inst, Dept Mech Engn, Madanapalle 517325, Andhra Pradesh, India;

    Natl Inst Technol Silchar, Dept Mech Engn, Silchar, Assam, India;

  • 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

    scramjet; Cavity geometry; Fuel injector location; Dual cavity; Mixing augmentation;

    机译:超燃冲压发动机;腔体几何形状;喷油嘴位置;双腔;混合增强;
  • 入库时间 2022-08-18 04:19:49

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号