Reynolds number effects on flow topology above blunt-edge delta wing VFE-2 configurations
This paper discusses further the effects of Reynolds number, angle of attack and leading edge bluntness on the flow topology above delta wing VFE-2 configurations. In this project two delta wing models differentiated by its leading edge radius to the mean aerodynamics chord ratio of 0.15 and 0.3, na...
Saved in:
Main Authors: | , , , , |
---|---|
Format: | Conference or Workshop Item |
Published: |
2015
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/60586/ https://pure.utm.my/en/publications/reynolds-number-effects-on-flow-topology-above-blunt-edge-delta-w |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|