Flight dynamics parameter estimation of a rotary wing aircraft using the output error minimization with natural and meta heuristic methods
I. Y. Sumida, H. F. de Campos Velho, E. F. P. Luz, R. V. Cruz and L. C. S. Goes*

Solid propellant rocket nozzle design and validation using Finite Difference Method and CFD technique
G. Imbrioscia, L. F. Barceló*, P. Vilar and M. Acuña

Assessment of openFoam solvers in aerospace applications
L. F.  Gutiérrez*, J. P.  Tamagno and S. A.  Elaskar

Reinjection probability density function for type-II and type-III intermittencies with Lower Boundary of Reinjection and noise
S. A. Elaskar* and E. del Río