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隐身进气道地面状态下流场结构

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为探明隐身进气道在地面状态下流场恶劣的原因,分别对三角形和M形等斜切口面进气道在地面状态下的流场结构进行数值仿真分析,并研究了唇口占比和内通道偏距对M形进口进气道地面工作特性的影响规律。结果表明:三角形口面进气道在进口对称面附近形成一个巨大的三维分离涡(一半流场),而M形口面进气道在侧唇口和上唇口交汇处形成一对尺度相对较小的旋涡,而且三角形口面进气道出口畸变指数过大,难以满足进/发匹配要求。随着M形口面唇口占比的增加,进气道出口截面低总压区沿着侧壁逆时针偏转,并且涡旋方向发生改变,总压恢复系数逐渐增大,畸变指数先减小后增加。内通道偏距的增大会进一步加剧地面状态下流场的恶化。
Flow field structure of stealth inlet under ground state
In order to find out the cause of bad flow field of the stealthy inlet under the ground state,the flow field structure of the triangular and M-shaped inlets with equal inclined cut surface under the ground state was numerically simulated and analyzed,and the influences of the lip ratio and internal channel offset on the ground working characteristics of the M-shaped inlet were studied.The results showed that a large three-dimensional separated vortex(half flow field)was formed near the inlet symmetry plane in the triangular inlet,while a pair of relatively small vortices were formed at the intersection of the side lip and the upper lip in the M-shaped inlet.Moreover,the distortion index at the outlet of the triangular inlet was too large to meet the inlet/engine matching requirements.With the increase of the proportion of the M-shaped lip,the low total pressure area of the inlet exit section deflected counterclockwise along the sidewall,and the direction of the vortex changed.The total pressure recovery coefficient gradually increased,and the distortion index decreased first and then increased.The increase of internal channel offset could further aggravate the deterioration of flow field under ground conditions.

inclined cut surface inletground working statethree-dimensional separated vortexflow field structuredistortion index

赵庆伟、谢文忠、李腾飞

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南京航空航天大学能源与动力学院,南京 210016

北京动力机械研究所高超声速冲压发动机技术重点实验室,北京 100074

斜切口面进气道 地面工作状态 三维分离涡 流场结构 畸变指数

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(11)