期刊
AIAA JOURNAL
卷 -, 期 -, 页码 -出版社
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J060090
关键词
-
资金
- Department of Defense High Performance Computing Modernization Program - Air Force Office of Scientific Research [88ABW-2020-2399]
- Air Force Office of Scientific Research
High-fidelity, time-accurate solutions of the flowfield around the HIFiRE-5 wind-tunnel geometry including postshock perturbations were obtained using the Overflow computational-fluid-dynamics solver. The time-averaged results show that the method reproduces the heat-flux contours measured experimentally via thermal imaging for both quiet and noisy facilities. This method has the potential to accurately extrapolate wind-tunnel tests between facilities and potentially to flight, and can also be used as a transition prediction method for flow conditions that cannot be accessed in existing ground facilities.
High-fidelity, time-accurate solutions of the flowfield around the HIFiRE-5 wind-tunnel geometry including postshock perturbations were obtained using the Overflow computational-fluid-dynamics solver. The time-averaged results show that the method reproduces the heat-flux contours measured experimentally via thermal imaging for both quiet and noisy facilities. Time-accurate results allow for the examination of transition phenomena and generation of computational disturbance spectra. It is shown that high-fidelity solutions reproduce the physics measured in experimental testing, and have the potential to serve as a method to accurately extrapolate wind-tunnel tests between facilities, and potentially to flight. The methods presented may also be used as a transition prediction method for flow conditions that cannot be accessed in existing ground facilities.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据