Validation of Flows on High-Lift Configurations by Structured- and Unstructured- Mesh Method
Turbulent Flow Solver Validation of FaSTAR and UPACS (AIAA 2014-0240)
Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR
Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel
Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop
Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing
High-Quality Unstructured Hybrid Mesh Generation for Capturing Effects of Vortex Generators
Experiment and CFD of a High-Lift Configuration Civil Transport Aircraft Model
EFFICIENT OPTIMIZATION DESIGN METHOD USING KRIGING MODEL
Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing
Efficient CFD Evaluation of Small Device Locations with Automatic Local Remeshing
DRAG PREDICTION ON NASA CRM USING AUTOMATIC HEXAHEDRA GRID GENERATION
Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid Solvers
CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model
AIAA 2006-1396 Comparison of RANS Simulations of Multi-Element High-Lift Configurations