期刊
AIAA JOURNAL
卷 53, 期 9, 页码 2504-2511出版社
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J053529
关键词
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资金
- High Performance Computing Center Stuttgart (HLRS) [GCS-Lamt 44026]
The influence of forward-facing steps on the amplification of disturbances in transonic flows is studied numerically. The main goal is to find a function for an additional amplification factor N that can be incorporated into the eN method. In the present study, both two-dimensional direct numerical simulation of disturbances as well as linear stability theory are used to gain detailed information on the flow. Good agreement between N-factor results from direct numerical simulation and linear stability theory is obtained. Subsonic and slightly supersonic results show differences in the flow topology and in the shape of the N-factor curve, but effective N factors are in the same order of magnitude.
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