Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop
Turbulent Flow Solver Validation of FaSTAR and UPACS (AIAA 2014-0240)
High-Quality Unstructured Hybrid Mesh Generation for Capturing Effects of Vortex Generators
Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR
Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid Solvers
AERODYNAMIC INFLUENCE OF A HALF-SPAN MODEL INSTALLATION FOR HIGH-LIFT CONFIGURATION EXPERIMENT
DRAG PREDICTION ON NASA CRM USING AUTOMATIC HEXAHEDRA GRID GENERATION
Evaluation of Computations and Transition Prediction Method for Aircraft High-Lift Configuration
Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel
2008-01-0423 Status of FCV Development at Nissan and Future Issues
Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing
Comparison Study of Drag Prediction by Structured and Unstructured Mesh Method
Status of FCV Development at Nissan and Future Issues
Efficient CFD Evaluation of Small Device Locations with Automatic Local Remeshing
Efficient Design Exploration of Nacelle Chine Installation in Wind Tunnel Testing