Robust Design Optimization of Supersonic Biplane Airfoil Using Efficient Uncertainty Analysis Method for Discontinuous Problem.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Jan2024, Vol. 11 Issue 1, p64, 21p
- Subject
AEROFOILS ROBUST optimization BIPLANES MONTE Carlo method MACH number DRAG coefficient POLYNOMIAL chaos - Language
- ISSN
- 22264310