A study investigated numerically the case when an incident shock wave propagated in a duct. The computational domain was two-dimensional, and computations were performed using a compressible inviscid flow model, solving the Euler equations. Computations were conducted for compressible flows inside the two-dimensional duct. In all computations, the duct was filled with air, while different gases filled the cavity. The same initial pressure prevailed in the duct and in the cavity.
ASJC Scopus subject areas
- Aerospace Engineering