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

Table 2

Static derivative calculation with traditional method.

Angle of attack (degree)	Steady at	Steady at
0; 5; 10; 15	0.0095261; 0.0196695; 0.0356153; 0.048699	0.0072; 0.0175805; 0.0330568; 0.0470066	0.1331; 0.1197; 0.1466; 0.097