Numerical investigation with experimental validation of aerodynamics performance of NACA 2414 airfoil with passive momentum injection through channeling
The aerodynamics of a segmented airfoil was investigated through two-dimensional (2D)-based computational fluid dynamics (CFD) simulations. The airfoil was segmented without changing its fundamental shape, letting secondary flows from its lower surface energize the upper surface. This method was to...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2025-03-01
|
| Series: | Results in Engineering |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2590123025006103 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|