Investigation of the vortical flow around a reverse delta wing
A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta...
| Main Authors: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2011
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/1/paper_4.pdf |
| Summary: | A six component force balance was used to obtain the
CL for a reverse delta wing and a delta wing for comparison
purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing. |
|---|