Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop
Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid Solvers
High-Quality Unstructured Hybrid Mesh Generation for Capturing Effects of Vortex Generators
Turbulent Flow Solver Validation of FaSTAR and UPACS (AIAA 2014-0240)
Validation of Flows on High-Lift Configurations by Structured- and Unstructured- Mesh Method