Uncertainty Quantification of Dynamic Stall Aerodynamics for Large Mach Number Flow around Pitching Airfoils
During high-speed forward flight, helicopter rotor blades operate across a wide range of Reynolds and Mach numbers. Under such conditions, their aerodynamic performance is significantly influenced by dynamic stall—a complex... | Find, read and cite all the research you need on Tech Science Press
Authors
- Guangjing Huang
- Zheng‐Hong Huang (ORCID: https://orcid.org/0000-0002-0591-6830)
- Fei Xiao (ORCID: https://orcid.org/0000-0003-3936-1631)
- Yunfeng Han (ORCID: https://orcid.org/0000-0002-0283-0505)
- Yuting Dai
Publication Details
- Journal
- Fluid dynamics & materials processing
- Published
- 2025-01-01
- DOI
- https://doi.org/10.32604/fdmp.2025.067528
- Primary Topic
- Probabilistic and Robust Engineering Design
- Type
- article
- Field-Weighted Citation Impact
- 0.00