Abstract
In this paper, a hybrid numerical flux scheme of low diffusion ECUSP (LDE) and HLL scheme is proposed by decomposing the cell-face normal vector. In the direction normal to shocks, the HLL scheme is applied to suppress carbuncles, in the other direction, the ECUSP scheme is implemented to keep low numerical diffusion. The new scheme with fifth-order WENO reconstruction is tested by using several benchmark cases, and then is applied to simulate a three dimensional double cone hypersonic flow of Mach number 12.43. The numerical simulation results agree very well with experiments.
| Original language | English (US) |
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| Title of host publication | 20th AIAA Computational Fluid Dynamics Conference 2011 |
| State | Published - Dec 1 2011 |
| Event | 20th AIAA Computational Fluid Dynamics Conference 2011 - Honolulu, HI, United States Duration: Jun 27 2011 → Jun 30 2011 |
Publication series
| Name | 20th AIAA Computational Fluid Dynamics Conference 2011 |
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Other
| Other | 20th AIAA Computational Fluid Dynamics Conference 2011 |
|---|---|
| Country | United States |
| City | Honolulu, HI |
| Period | 6/27/11 → 6/30/11 |
ASJC Scopus subject areas
- Fluid Flow and Transfer Processes
- Energy Engineering and Power Technology
- Aerospace Engineering
- Mechanical Engineering
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Cite this
Shen, Y., Zha, G., & Huerta, M. A. (2011). Rotated hybrid low diffusion ecusp-hll scheme and its applications to hypersonic flows. In 20th AIAA Computational Fluid Dynamics Conference 2011 (20th AIAA Computational Fluid Dynamics Conference 2011).