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