力学学报(英文版)2024,Vol.40Issue(1) :74-84.DOI:10.1007/s10409-023-23135-x

后缘开槽型超燃冲压发动机凹腔燃烧室及其促燃特性实验研究

Experimental study of scramjet cavity with rear edge slots and its performance in combustion enhancement

张林 乔竑玮 梁剑寒 王翼 丁猛 杨雷超 孙明波
力学学报(英文版)2024,Vol.40Issue(1) :74-84.DOI:10.1007/s10409-023-23135-x

后缘开槽型超燃冲压发动机凹腔燃烧室及其促燃特性实验研究

Experimental study of scramjet cavity with rear edge slots and its performance in combustion enhancement

张林 1乔竑玮 1梁剑寒 1王翼 1丁猛 1杨雷超 1孙明波1
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作者信息

  • 1. Science and Technology on Scramjet Laboratory,National University of Defense Technology,Changsha 410073,China
  • 折叠

摘要

为了改善传统的二维梯形凹腔在促进混合和燃烧方面的效果,本文提出了一种在凹腔后缘设置开槽的三维凹腔,并在超声速模型燃烧室中进行了研究.在直连式实验台上开展实验,对传统的二维梯形凹腔(基线)和后缘开槽凹腔进行了对比.结果表明,后缘开槽凹腔增强了沿燃烧室的燃烧.具体而言,凹腔附近的压力在燃料喷注压力较低时增加6.1%,在燃料喷注压力较高时增加12.7%.基于准一维分析,后缘开槽凹腔的燃烧效率提高了20%以上.对于后缘开槽凹腔,燃烧面积和火焰基底位置受喷注压力的影响小于基线情况.与此同时,后缘开槽凹腔的火焰稳定能力较基线构型更优.凹腔交换面积增加、长深比增大以及开槽诱导的横向流动和流向涡可能是增强混合和燃烧的主要原因.

Abstract

To improve the effect of the traditional two-dimensional trapezoidal cavity in promoting mixing and combustion,a three-dimensional cavity with slots equipped on the cavity rear edge was proposed and investigated in a model supersonic combustor in this work.Experiments are conducted at a direct-connect test facility,where the traditional two-dimensional trapezoidal cavity(baseline)case and the slots cavity case are compared.The results show that the overall combustion along the combustor is intensified by the slots cavity.Specifically,the wall static pressure around the cavity increases by 6.1%at the lower injection pressure and 12.7%at the higher injection pressure.Based on the quasi-one-dimensional analysis,the estimated combustion efficiency increases by more than 20%due to the slots cavity.For the slots case,the combustion area and flamebase location are less affected by the injection pressure than that for the baseline case.As a result,the combustion that the slots cavity stabilizes is more stable than the combustion that the baseline cavity stabilizes.The increased exchange area,the bigger length-to-depth ratio,and the transverse flow and streamwise vortices induced by the slots may be responsible for the enhanced mixing and combustion.

关键词

Supersonic combustor/Cavity configuration/Slots/Combustion enhancement

Key words

Supersonic combustor/Cavity configuration/Slots/Combustion enhancement

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基金项目

国家自然科学基金(12202487)

国家自然科学基金(11972367)

出版年

2024
力学学报(英文版)

力学学报(英文版)

CSTPCD
影响因子:0.363
ISSN:0567-7718
参考文献量33
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