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Updated: Jul 2, 2025

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A Rapid Method for Modeling a Variable Cycle Engine
Published on: August 13, 2019
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气体运动方案与超音速过渡流量模拟的高速修改相结合
Chengrui Li1, Wenwen Zhao1,2, Hualin Liu3
1School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
Entropy (Basel, Switzerland)
|February 23, 2024
概括
这项研究引入了一种先进的介光学方法,用于预测高超音速边界层过渡. 合气体运动方案和兰特里-门特模型提高了高速车辆设计的准确性.
科学领域:
- 航空航天工程 航空航天工程
- 计算流体动力学的流体动力学.
- 高速空气动力学 高速空气动力学
背景情况:
- 准确预测超音速边界层过渡对于高速车辆设计至关重要.
- 现有的方法可能缺乏复杂的高速流体现象所需的保真度.
研究的目的:
- 开发和验证用于高超音速边界层过渡预测的先进的中视镜方法.
- 为了提高Langtry-Menter过渡模型对高速流动的预测能力.
主要方法:
- 将气体运动方案 (GKS) 与Langtry-Menter过渡模型相合,包括其高速修改.
- 将流动动能纳入马克斯韦尔速度分布函数的中观层面.
- 通过超音速平板,高超音速圆和HIFiRE飞行试验案例验证GKS合的美索斯科普方法.
主要成果:
- 与GKS相结合的中视镜方法在各种测试案例中与实验数据表现出良好的一致性.
- 与传统的戈杜诺夫方法相比,新方法捕获了更广泛的物理机制.
- 计算结果与真正的物理现象密切一致,显示出更高的准确性和准确性.
结论:
- 开发的中视镜方法为预测高超音速边界层过渡提供了准确而快速的解决方案.
- 这种创新方法满足了对高速车辆空气动力学设计中可靠工具的工程需求.
- 该方法的增强预测能力对实际工程应用具有重大潜力.
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