An Evaluation of the Dynamics and Handling Quality Characteristics of the Bell 412 HP Helicopter
Airflow Angle Measurement Using a Multi-hole Radome Differential Pressure Technique
Simultaneous Calibration of Aircraft Position Error and Airflow Angles Using Differential GPS
Flight Testing and Simulator Model Development for the De Havilland Dash 8 Aircraft
An Improved Aerodynamic Model of a Bell 205 in Forward Flight
NRC-IAR and CAE: Collaboration in the Area of Flight Testing and Simulator Model Development