Motivation: Is PINN as accurate as conventional CFD in compressible flows where shock waves occur?
PINN derives results by training a neural network to satisfy the governing equations and boundary conditions applied to the domain of interest.
Sod Shock Tube Problem
*Contributor: Jun-sang Yoon (Feb 2026)*
Quasi-1D Nozzle Flow
*Contributor: Seung-Hyun Choi (Feb 2026)*
Supersonic Shock Wave Around a Corner
*Contributor: Jae-won Yu (Feb 2026)*