Design Optimization of Subcavitating Hydrofoils for America's Cup Class Yachts - presented by Prof. Joaquim R. R. A. Martins

Design Optimization of Subcavitating Hydrofoils for America's Cup Class Yachts

Prof. Joaquim R. R. A. Martins

Prof. Joaquim R. R. A. Martins
Slide at 23:27
MACH is a framework for aerostructural optimization
2: Baseline design
3: FFD points
4: Aerodynamic mesh
5: Structural mesh
2. 10->3:
3: Updated FFD
5: Updated structural
Optimizer
displacement
sizing variables
11: Geometric
3: Geometry
4: Updated aero
constraints and
parameterization
surface coordinates
derivatives
4: Volume mesh
5: Updated
deformation
aerodynamic mesh
11: Values of
5,9-6:
6: Structural
10: Converged
objectives and
Aerostructural
aerostructural
displacement
constraints
solver
state variables
6: Volume mesh
7: Deformed
deformation
aero mesh
9: Aerodynamic
8: Surface
7: Flow solver
state variables
pressure
9: Structural
8: Structural solver
state variables
11: Derivatives
of objectives &
10: Coupled adjoint solver
constraints
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Summary (AI generated)

The current analysis involves a coupled adjoint approach that accounts for the interaction between aerodynamic and structural elements. This framework includes both a structural adjoint and an aerodynamic adjoint, along with off-diagonal terms to facilitate full coupling. A prototype of this methodology was first developed during my PhD thesis at Stanford, in collaboration with James Reuter and Juan. This project marked the initial integration of Computational Fluid Dynamics (CFD) within the optimization loop.

In hydrostatic applications, the scenario differs from traditional wing box configurations, as we are dealing with solid structures. Consequently, the elements utilized are solid elements. In this context, the outer mold line serves as a structural variable; adjustments to the outer mold line directly impact the structure. This relationship is akin to that of a wing box but exhibits even greater influence due to the absence of thickness variables.