New Systematic CFD Methods to Calculate Static and Single Dynamic Stability Derivatives of Aircraft

Table 1

Static derivative calculation with new method.

Angle of attack (degree)	Unsteady	Steady
0; 5; 10; 15	0.01012; 0.02100; 0.036825; 0.04847	0.008590; 0.019143; 0.034687; 0.0481005	0.15339; 0.1762; 0.2138; 0.0376