FULL-LENGTH PAPERS - Automated Method for Transition Prediction on Wings in Transonic Flows
Fully Three Dimensional Transition Prediction on Swept Wings in Transonic Flows
NSU3D Results for the Second AIAA High-Lift Prediction Workshop
A Linear Stability Analyser Suitable for Integration in Wing Performance Calculation Procedures
NSU3D Results for the Second High-Lift Prediction Workshop (AIAA 2014-0748)
Transition Prediction Capabilities for Conical Wings in the Transonic Regime
Curvature and Nonparallel Effects in 3-D Compressible Transition Analysis
"Transition Prediction and Correlation on Bombardier Wings"
Non-Parallel Effects in Stability Analysis by the PSE Approach
Investigation of a Multi-Element Airfoil High-Lift Characteristics at High Reynolds Numbers
Use of Navier-Stokes Methods for Analysis of High-Lift Systems
A Linear Stability Analyser Suitable for Integration in Wing Performance Calculation Procedures
Two-Dimensional Transition Predictions - Comparison with Experiments