Stability and Control Derivatives of the De Havilland DHC-2 'BEAVER' Aircraft

摘要

The report presents a database of stability derivatives of the De Havilland DHC-2 'BEAVER' experimental aircraft of the Delft University of Technology at various stationary nominal flight conditions. To compute these stability derivatives a nonlinear aerodynamic model is used. The flight test data of this model is based on data derived from the DHC-2 'BEAVER' test flights of the 1977/1978 period. The stability derivatives are presented at several nominal flight conditions throughout the normally used flight envelope of the aircraft.