Optimization Solver
Airfoil Shape Optimization Using Surrogate model & QIO
Achieved high-accuracy drag prediction with R² = 0.996 and improved design convergence|| Faster exploration • Reduced evaluation cost • Stable optimization
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Before acceleration, the QA-PINN workflow faced a major compute bottleneck:
Key limitation: training time, not algorithm capability.

Running QA-PINN on CUDA-Q delivered a substantial performance leap:
The solver became significantly more practical for real CFD workloads

85 hours to 3.5 hours using CUDA-Q on A100 GPU.



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