1. Simulation of the flow over elliptic airfoils oscillating at large angles of attack;Akbari;Journal of Fluids and Structures,2000
2. Simulation of dynamic stall for a NACA 0012 airfoil using a vortex method;Akbari;Journal of Fluids and Structures,2003
3. Benetka, J., Kladrubský, J., Valenta, R., 1998. Measurement of NACA 0012 profile in a slotted measurement section. Technical Report R-2909/98, Aeronautical Research and Test Institute, Prague, Letňany (in Czech).
4. Čečrdle, J., Maleček, J., 2002. Verification FEM model of an aircraft construction with two and three degrees of freedom. Technical Report R-3418/02, Aeronautical Research and Test Institute, Prague, Letňany (in Czech).
5. A combined unifrontal/multifrontal method for unsymmetric sparse matrices;Davis;ACM Transactions on Mathematical Software,1999