Journal of Theoretical
and Applied Mechanics
21, 2-3, pp. 481-492, Warsaw 1983
and Applied Mechanics
21, 2-3, pp. 481-492, Warsaw 1983
Numeryczna symulacja korkociągu samolotu
A method of digital computer simulation for an aircraft in spin is presented. Differential motion equations have been established for a rigid airplane having six degrees of freedom. Deflections of control surfaces were assumed to have an influence only on aerodynamic forces and moments. Test calculations were carried out for Polish training aircraft TS-11 ,,Iskra''.