Local correlation-based transition model for aerodynamic flows in wide speed range
A local correlation-based transition model is developed for aerodynamic flows in a wide speed range. New localized methods for the momentum-thickness Reynolds number are introduced for constructing local transition indicators. New transition correlations are developed to detect transition in high-sp...
Saved in:
| Main Authors: | Hexia Huang, Zaijie Liu, Huijun Tan |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Taylor & Francis Group
2025-12-01
|
| Series: | Engineering Applications of Computational Fluid Mechanics |
| Subjects: | |
| Online Access: | https://www.tandfonline.com/doi/10.1080/19942060.2024.2442738 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
The Effect of Turbulent Intensity on Friction Coefficient in Boundary-Layer Transitional Flat Plate Flow
by: Muhsine Saru, et al.
Published: (2025-05-01) -
Effect of Mach Number on Stability of Boundary Layer Over a Rotating Cone in Hypersonic Flow
by: Yiyang GU, et al.
Published: (2025-05-01) -
Symbolic regression modelling of the linear growth rates of stationary cross-flow instabilities
by: Lucas Pascal
Published: (2025-01-01) -
Porous Surface Design with Stability Analysis for Turbulent Transition Control in Hypersonic Boundary Layer
by: Youngwoo Kim, et al.
Published: (2025-06-01) -
Analysis of Influencing Factors of Boundary Layer Transition During Ascent Phase of Hypersonic Vehicle
by: Yiwei TANG, et al.
Published: (2024-11-01)