One of the Stanford’s experiments has been specifically designed to assess the quality of various UQ propagation methods

This is a unique component of this program

Prof. Eaton’s Shock/Boundary layer interaction test will include features to accurately control the inflow turbulence and boundary geometry.

Physical Monte Carlo
100 to 1000 repeated measurements will be used to build detailed sensitivity maps and PDFs of important quantities such as separation length, shock locations.

Individually adjustable pins for surface geometry perturbation