A robust and high-fidelity aerodynamic optimization design of truss-braced-wing aircraft with gradient-based method
- Type
- Retraction
- Notice date
- 8/14/2019 0:00
- Journal
- Aerospace Science and Technology
- Publisher
- Elsevier
- Notice DOI
- 10.1016/j.ast.2019.105338
- Original paper DOI
- 10.1016/j.ast.2019.105338