Flow control mechanism of sprays using dual synthetic jets
Dual Synthetic Jets (DSJ) can directly affect the development of spray through the complex vortex structure. The mechanism of flow control on spray and its thermal management application are studied by combining experiment and simulation. The spray characteristics under different injection angles are studied, and the results show that the angle should be controlled in the range of 45°–60°, so that sufficient momentum transfer can be obtained, and meanwhile spray impingement area narrowing can be avoided. The spray characteristics under flow control of DSJ with different Reynolds numbers are studied, and the results show that Reynolds number should be controlled in the range of 2859–3574, so that strong particle streamwise acceleration and wall film disturbing can be achieved. In addition, the DSJ kinetic energy is utilized more efficiently. On the basis of previous research, this paper proposes a novel active heat pipe based on spray controlled by DSJ. The space occupancy has been reduced by more than 60%. Even in a sealed state, the active heat pipe is able to cool a hot surface with heat flux of 22.2 kW/m 2 from 111 °C to 57 °C only in 20 s. The noise of DSJ is reduced from 85 dB to 60 dB, which is expected to promote the practical application of DSJ in thermal management.
Authors
- Songjiang Feng
- Sheng Xu (ORCID: https://orcid.org/0000-0002-7503-2467)
- Xiong Deng (ORCID: https://orcid.org/0000-0001-6885-6188)
- L. Xia (ORCID: https://orcid.org/0000-0001-9198-1497)
- Zhenbing Luo (ORCID: https://orcid.org/0000-0003-1009-2706)
- Sen Li (ORCID: https://orcid.org/0000-0001-7850-1866)
- Wei He (ORCID: https://orcid.org/0009-0007-2546-9111)
Institutions
- National University of Defense Technology (CN)
- Space Engineering University (CN)
Publication Details
- Journal
- Chinese Journal of Aeronautics
- Published
- 2024-12-20
- DOI
- https://doi.org/10.1016/j.cja.2024.103362
- Citations
- 4
- Primary Topic
- Plasma and Flow Control in Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 5.20
Funders
- National Natural Science Foundation of China