A BEM Adjoint-Based Differentiable Shape Optimization of a Stealth Aircraft
Modern fighter aircraft have an increasing need for at least a moderate level of stealth, and the shape design must bear a part of this constraint. However, the high frequency of close range radar makes high-fidelity radar cross-section computation methods such as the boundary element method too exp...
Saved in:
| Main Authors: | Charles Thoulon, Gilbert Roge, Olivier Pironneau |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-07-01
|
| Series: | Eng |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2673-4117/6/7/147 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Aerodynamic Shape Optimization of Wing–Fuselage Intersection for Minimum Interference Drag
by: Nuno M. B. Matos, et al.
Published: (2025-04-01) -
Hydrodynamic Shape Optimization of a Naval Destroyer by Machine Learning Methods
by: Andrea Serani, et al.
Published: (2024-11-01) -
Recent Advances in Optimization Methods for Machine Learning: A Systematic Review
by: Xiaodong Liu, et al.
Published: (2025-07-01) -
A Gradient Enhanced Efficient Global Optimization-Driven Aerodynamic Shape Optimization Framework
by: Niyazi Şenol, et al.
Published: (2025-07-01) -
Shape design for controlling structural displacement distribution in unsteady fluid-structure-interaction
by: Shota NARUSE, et al.
Published: (2025-03-01)