VERIFICATION OF THE TURBULENCE MODEL IN THE SIMULATION OF THE FLOW AROUND THE PROPELLER OF A BIPLANE
The paper presents the results of a physical and numerical experiment to measure the thrust generated by a UAV propeller. The analysis of the results shows that the discrepancy between the results of the physical and numerical experiments ranges from 1 to 12%
Institutions
- National University "Kyiv Aviation Institute" (UA)
Publication Details
- Journal
- Zenodo (CERN European Organization for Nuclear Research)
- Published
- 2025-02-27
- DOI
- https://doi.org/10.5281/zenodo.14937530
- Primary Topic
- Biomimetic flight and propulsion mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 0.00