Multi-objective aerodynamic optimization of flying-wing configuration based on adjoint method
In order to solve the multi-objective multi-constraint design in aerodynamic design of flying wing, the aerodynamic optimization design based on the adjoint method is studied. In terms of the principle of the adjoint equation, the boundary conditions and the gradient equations are derived. The Navie...
| Format: | Article |
|---|---|
| Language: | zho |
| Published: |
EDP Sciences
2021-08-01
|
| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/04/jnwpu2021394p753/jnwpu2021394p753.html |