The computation of the pitch damping stability derivatives of supersonic blunt cones using unsteady sensitivity equations
Abstract The numerical methods for computing the stability derivatives of the aircraft by solving unsteady sensitivity equations which was proposed in our previous papers was extended to solve three-dimensional problems in this paper. Both the static and dynamic derivatives of the hypersonic blunt c...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
SpringerOpen
2019-07-01
|
| Series: | Advances in Aerodynamics |
| Subjects: | |
| Online Access: | http://link.springer.com/article/10.1186/s42774-019-0018-3 |