The Influence of Ice Accretion on the Thermodynamic Performance of a Scientific Balloon: A Simulation Study
A scientific balloon is the ideal platform for carrying out long-duration missions for scientific research in the stratosphere. However, when a scientific balloon ascends through icy clouds and reaches supercooled droplets, there is a risk of ice accretion on the balloon’s surface. Ice accretion on the balloon can threaten flight safety and the accomplishment of missions and can even result in disastrous accidents. A comprehensive simulation platform was developed to simulate the influence of ice accretion on the thermodynamic performance of a scientific balloon to provide quantitative data support for balloon design and flight operations. The simulation platform consisted of two parts: one based on ANSYS software to solve the accretion model and the other a program developed with MATLAB software to solve the thermodynamic model. The results suggest that, in certain cloud environments, there is a risk of ice accretion on a balloon’s surface; the extra ice mass added to the balloon may prevent it from ascending through icy clouds and instead keep it floating at the base of these clouds.
Authors
- Rongchen Zhu
- Kang Zhao (ORCID: https://orcid.org/0000-0002-8321-2804)
- Qiang Liu (ORCID: https://orcid.org/0000-0002-5302-9849)
- Tao Li (ORCID: https://orcid.org/0000-0001-8958-1355)
- Yanchu Yang
- Lan He (ORCID: https://orcid.org/0000-0001-6744-9812)
- Yanqing Wang
Institutions
- Chinese Academy of Sciences (CN)
- Aerospace Information Research Institute (CN)
- University of Chinese Academy of Sciences (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2024-10-31
- DOI
- https://doi.org/10.3390/aerospace11110899
- Citations
- 2
- Primary Topic
- Icing and De-icing Technologies
- Type
- article
- Field-Weighted Citation Impact
- 2.60
Funders
- Youth Innovation Promotion Association of the Chinese Academy of Sciences