Subsonic dynamic stability experiment on the anti-tank missile model
One of the most difficult aspects of aircraft and missile development is defining stability and control characteristics. The best way to obtain model-scale dynamic stability derivatives is to perform experiments in wind tunnels having high Reynolds number. In the T-38 wind tunnel the forced oscillat...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2013-01-01
|
| Series: | FME Transactions |
| Subjects: | |
| Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2013/1451-20921302114S.pdf |