Evolution of the surface flow topology on a 65° delta wing and its correspondence to the critical states, AIAA 2000-790
Evolution of the surface flow topology on a 65° delta wing and its correspondence to the critical states, AIAA 2000-790
DOI | Resolve DOI: https://doi.org/10.2514/6.2000-790 |
---|---|
Author | Search for: 1; Search for: 1 |
Affiliation |
|
Format | Text, Article |
Conference | 38th Aerospace Sciences Meeting and Exhibit, January 10-13, 2000, Reno, Nevada, USA |
Subject | leading-edge vortex; high angle of attack |
Publisher | American Institute of Aeronautics and Astronautics |
In | |
Peer reviewed | Yes |
NRC number | AL-2000-0083 |
NPARC number | 8926628 |
Export citation | Export as RIS |
Report a correction | Report a correction (opens in a new tab) |
Record identifier | ddec058b-9a8d-4c84-99db-437f41281cf4 |
Record created | 2009-04-23 |
Record modified | 2020-04-16 |
- Date modified: