TY  - JOUR
PY  - 2016//
TI  - Analysis of stability derivatives important to recovery from spin
JO  - Aviation
A1  - Figat, Marcin
A1  - Goraj, Zdobysław
SP  - 48
EP  - 52
VL  - 20
IS  - 2
N2  - This paper describes the numerical analysis of light aircraft stability derivatives in a wide range of angles of attack, important for recovery from spin. Stability derivatives versus angle of attack and sideslip were calculated using a CFD software, based on Euler equation combined with boundary layer equations. The analysis was performed up to the 40 deg of angle of attack and up to 25 deg of sideslip.<p />  <p>Language: en</p>
LA  - en
SN  - 1648-7788
UR  - http://dx.doi.org/10.3846/16487788.2016.1195060
ID  - ref1
ER  -