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

Table 3

Static derivative results.

Angle of attack (degree)	Calculation results	Reference data [17]	Traditional method
0; 5; 10; 15	0.15339; 0.1762; 0.2138; 0.0376	0.15450; 0.1722; 0.2079; Not given	0.1331; 0.1197; 0.1466; 0.097