Numerical Investigation of the Non-Uniform Distribution of Outlet Parameters in a Radial Wave Rotor Combustor
The non-uniform distribution of outlet parameters in a Radial Wave Rotor Combustor (RWRC) significantly impacts downstream component performance. This study aims to investigate the spatial-temporal characteristics of temperature and pressure at the RWRC outlet. Three-dimensional unsteady Reynolds-Averaged Navier–Stokes (RANS) simulations were coupled with a User-Defined Function (UDF) to efficiently model the combustion process. The Shear-Stress Transport (SST) k-ω turbulence model was employed. Quantitative metrics including Relative Standard Deviation (RSD) and Christiansen Uniformity Coefficient (CUC) were introduced to evaluate the non-uniformity. The results reveal significant temporal fluctuations and spatial non-uniformity in both temperature and pressure. At 3000 r/min, the average temperature fluctuation amplitude and uniformity coefficient are 0.38 and 0.9, respectively, while the pressure fluctuation amplitude reaches 0.44. Crucially, temperature distribution expands circumferentially with increasing speed, whereas pressure distribution remains locally concentrated and is less sensitive to speed variations. This study provides a quantitative assessment of outlet non-uniformity in RWRC, highlighting the distinct behaviors between temperature and pressure distributions. The findings offer critical insights for the design and optimization of wave rotors and their integration with downstream components.
Authors
- Qian Yao (ORCID: https://orcid.org/0000-0003-4245-7095)
- Erlei Gong
- Ji‐Zhao Liang (ORCID: https://orcid.org/0009-0003-4756-4866)
- Jianzhong Li (ORCID: https://orcid.org/0009-0008-2075-0219)
- Wu Jin
Institutions
- Changzhou Institute of Technology (CN)
- Nanjing University of Aeronautics and Astronautics (CN)
Publication Details
- Journal
- Energies
- Published
- 2025-10-24
- DOI
- https://doi.org/10.3390/en18215588
- Primary Topic
- Combustion and Detonation Processes
- Type
- article
- Field-Weighted Citation Impact
- 0.00