1. Li SX. Hypersonic flow characteristics of typical configuration. Beijing: National Defense Industry Press; 2007. p. 156–7.
2. Peebles C. The X-43A flight research program: Lessons learned on the road to Mach 10. Reston: AIAA Inc.; 2007. p. 23–4.
3. Walker S, Rodgers F. Falcon hypersonic technology overview. Reston: AIAA; 2005. Report No.: AIAA-2005-3253.
4. Gibson FW, Mixson JS. Flutter investigation at a Mach number of 7.2 of models of the horizontal- and vertical-tail surfaces of the X-15 airplane. Washington, D.C.: NASA; 1959, Report No.: NASA MEMO 4-14-59L.
5. Effects of leading-edge swept on flutter characteristics of some delta-planform surfaces at a Mach number of 15.4;Goetz,1964