1. E.C. Yates Jr., N.S. Land, J.T. Foughner Jr., Measured and Calculated Subsonic and Transonic Flutter Characteristics of a 45° Sweptback Wing Planform in Air and Freon-12 in the Langley Transonic Dynamic Tunnel, NASA Technical Note D-1616, 1963
2. SPECTRUM, Centric Technology, Inc., Sunnyvale, CA. Now owned by ANSYS
3. W. Wall, E. Ramm. A finite element based approach for nonlinear, unsteady fluid-structure interaction problems. in: Proceedings of the MAFELAP Conference on the Mathematics of Finite Elements and Applications, 1999, p. 130
4. Mixed explicit/implicit time integration of coupled aeroelastic problems: three field formulation, geometric conservation and distributed solution;Farhat;Int. J. Numer. Meth. Fluids,1995
5. High performance solution of three dimensional nonlinear aeroelastic problems via parallel partitioned algorithms: methodology and preliminary results;Farhat;Adv. Eng. Softw.,1997