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UC San Diego · Mechanical and Aerospace Engineering

Large-Scale Design Optimization Laboratory

We conduct fundamental research in large-scale multidisciplinary design optimization (MDO) to improve the design of complex engineering systems.

The Large-Scale Design Optimization Laboratory at UC San Diego develops novel computational methods, tests them on industrially relevant applications across aerospace and mechanical engineering, and creates open-source research software to enable researchers to use and extend our work.

Our primary focus is system-level, large-scale MDO: using numerical optimization to explore high-dimensional design spaces while considering the interactions among many disciplines and subsystems across multiple operating conditions.

Research applications

All applications →
Animation of the 15 modeled design conditions, including nominal flight, motor-failure, static structural-sizing, and quasi-steady transition cases. Source paper

Application

Lift-plus-cruise aircraft

Coupled aircraft sizing, mission analysis, and design under uncertainty.

Methods and publications →
01

Graph-native modeling

Generating model evaluations and derivatives from a common graph, with efficient execution for coupled and time-dependent physics.

02

Unsteady potential-flow adjoints

Differentiable potential-flow analysis with reduced memory costs for steady aircraft models and evolving aerodynamic wakes.

03

MDO under uncertainty

Reducing uncertainty-propagation cost through computational graph structure, response sensitivities, and dimension reduction for multidisciplinary design.

04

Distributed optimization

Coordinating disciplinary subproblems to manage memory, improve convergence, and satisfy shared design constraints.

05

Nonlinear programming

Using analysis convergence, directional curvature, and modular algorithms to improve the solution of coupled engineering design problems.

06

Projection-based model reduction

Adapting reduced simulation bases to changing designs while retaining the accuracy needed for structural and aerodynamic optimization.

07

Scientific machine learning

Combining physical models and sensitivity information with training data to predict spatial fields for engineering design.

08

Geometry parameterization

Connecting design variables to component geometry while preserving the dimensions and relationships that define a configuration.

09

Geometric non-interference constraints

Enforcing the component clearances needed for physically feasible configurations without impairing optimizer conditioning.

10

Mesh deformation

Updating aircraft analysis meshes through large shape and component-placement changes while retaining derivatives for gradient-based design.

11

Multiphysics coupling

Connecting disciplinary solvers through shared field representations and transfer operators that preserve the required physical relationships.