The solution of challenging multi-disciplinary problems involves the interaction between
separate modules that represent different physical models and procedures, and for avoiding …

This paper presents a comprehensive set of test cases for the verification and validation (V &
V) of the Stanford University Unstructured (SU2) software suite within the context of …

The effect of thermal nonequilibrium on shock interactions of carbon dioxide (CO 2)
hypersonic flows is investigated. Given the relatively low characteristic vibrational …

The present study aims at providing insights into shock wave interference patterns in gas
flows when a mixture different than air is considered. High-energy non-equilibrium flows of …

This work investigates shock interaction mechanisms in inviscid hypervelocity gas flows over
double-wedge geometries using computational fluid dynamics. The SU2 CFD solver has …

The presence of complex geometries and/or multiple bodies during atmospheric reentry may
lead to complex and directional flow features, such as shock waves and shear layers, that …

We demonstrate the power of adaptive mesh refinement with adjoint-based error estimates
in verification of simulations governed by the steady Euler equations. The flow equations are …

Predicting shock/shock and shock/boundary-layer interactions in gas flows that surround
high-speed vehicles is key in aerodynamic design. Under typical hypersonic conditions …

This is an investigation on two experimental datasets of laminar hypersonic flows, over a
double-cone geometry, acquired in Calspan—University at Buffalo Research Center's Large …

Mesh adaptation is often used to control errors and verify the performance of a design, which
can tell us if the objective was accurately predicted. Significant work has gone into validation …