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

Table 4

Translation acceleration derivative results.

Angle of attack (degree)	Unsteady at time of step motion with constant	Unsteady at time of step motion with constant	Calculation; results	Wind tunnel; testing [18]
0; 5; 10; 15	0.012749; 0.0249; 0.04125; 0.05326	0.01012; 0.02100; 0.036825; 0.04847	0.2629; 0.39; 0.4425; 0.479	Not given; Not given; 0.45; 0.5