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
AIAA 2006-1396 Comparison of RANS Simulations of Multi-Element High-Lift Configurations
2008-01-0423 Status of FCV Development at Nissan and Future Issues
Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel
DRAG PREDICTION ON NASA CRM USING AUTOMATIC HEXAHEDRA GRID GENERATION
AERODYNAMIC INFLUENCE OF A HALF-SPAN MODEL INSTALLATION FOR HIGH-LIFT CONFIGURATION EXPERIMENT
Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR
Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing
EFFICIENT OPTIMIZATION DESIGN METHOD USING KRIGING MODEL
CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model