1. Blades EL, Ruth M, Fuhrmann HD. Aeroelastic analysis of the X-34 Launch Vehicle. AIAA paper April 99;1999–135.
2. Holst TL, Flores J, Kaynak U, Chaderjian N. Navier–Stokes computations, including a complete F-16 Aircraft. Progress in Astronautics and Aeronautics, AIAA, vol. 125, ISBN 0-930403-69-X, 1990.
3. Finite element procedures;Bathe,1996
4. The finite element method;Zienkiewicz,1977
5. Felker FF. A new method for transonic aeroelastic problems. AIAA-92-2123, 1992.