采用射流掺混增强的前可调面积涵道引射器数值模拟
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中央高校基本科研业务费专项资金资助项目(20822041B4219)


Numerical investigation of front variable area bypass injector with jet mixing enhancement
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    摘要:

    为了提高风扇外涵和核心机驱动风扇级外涵流体的掺混效率,提出一种采用射流掺混增强的前可调面积引射器设计方案。通过数值模拟的手段对流量特性、流动掺混和总压损失等方面进行了研究,并同基准模型进行了对比分析,结果表明:采用波瓣混合器结构的前可调面积引射器设计,显著地增加了较高出口背压工况下风扇外涵的流通能力;新的设计方案不仅没有增加低出口背压工况下的总压损失,还减小了高背压出口工况下的流动损失;流向涡的特征尺度是提高掺混效率的关键,可以进一步优化波瓣混合器几何轮廓,以满足调节机构对结构设计的要求。

    Abstract:

    In order to improve the mixing performance of fan bypass and CDFS (core driven fan stage) bypass, a innovative configuration of FVABI (front variable area bypass injector) with jet mixing enhancement was proposed. Numerical simulation was performed to investigate mass flow rate characteristic, flow mixing and total pressure loss of FVABI configuration with lobed mixer. Compared with the baseline configuration, the predictions are discussed and several conclusions can be summarized. Firstly, the significant improvement in fan bypass mass flow rate is achieved by jet mixing enhanced configuration at high back pressure operating point. Secondly, the performance is not degraded at low back pressure operating situation, but the total pressure loss is decreased at high back pressure operating point. Finally, the characteristic length of stream-wise vortex is the key to improve mixing performance, and the optimization of lobed mixer is available to match further structural requirement of adjust configuration.

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王靖宇,张怀宝,黄国平,等.采用射流掺混增强的前可调面积涵道引射器数值模拟[J].国防科技大学学报,2019,41(2):69-74,81.
WANG Jingyu, ZHANG Huaibao, HUANG Guoping, et al. Numerical investigation of front variable area bypass injector with jet mixing enhancement[J]. Journal of National University of Defense Technology,2019,41(2):69-74,81.

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  • 收稿日期:2017-11-08
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  • 在线发布日期: 2019-04-24
  • 出版日期: 2019-04-28
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