Validation of Flows on High-Lift Configurations by Structured- and Unstructured- Mesh Method
Validation of Computations Around High-Lift Configurations by Structured- and Unstructured-Mesh
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
PIV Measurement of a High-Lift-Device Model in JAXA 6.5m x 5.5m Low-Speed Wind Tunnel AIAA Paper
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 of Airframe Noise from High Lift Configuration Model
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
High-Lift Device Testing in JAXA 6.5M x 5.5M Low-Speed Wind Tunnel
Experiment and CFD of a High-Lift Configuration Civil Transport Aircraft Model
Evaluation of Computations and Transition Prediction Method for Aircraft High-Lift Configuration
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