Measurements of Aerodynamic Stability Derivatives of an Airplane in Wind Tunnels
風洞における機体の安定微係数の測定法

Hiroshi MAEDA
1960 The Journal of the Japan Society of Aeronautical Engineering  
The two methods for determining the aerodynamic stability derivatives of an airplane in wind tunnels are investigated. The principles of measurements are as follows :
doi:10.2322/jjsass1953.8.215 fatcat:ticjquhl25bjdctfrelafpr5my