1. HirschelE. H.WeilandC., Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, Vol. 229, AIAA, Reston, VA, 2009, pp. 200–203.
2. RunyanH. L.MorganH. G. “Flutter at Very High Speeds,” NACA Rept. RML57D16a, 1957, pp. 1–15.
3. HurleyS. R. “Hypersonic Flutter Model Tests of Advanced Wing Configurations at Initial Angles of Attack,” Technical Documentary Rept. RTD-TDR-63-4219, Air Force Flight Dynamics Laboratory Research and Technology Division Air Force Systems Command, Wright-Patterson Air Force Base, OH, Project No. 1370, Task No. 137003, DOD DIR. 5200.10 Prepared Under Contract No. AF33(616)-7770, North American Aviation, Inc., Columbus, OH, Oct. 1964, pp. 1–174.
4. GoetzR. C.SewallJ. L. “Experimental Flutter Study of a Wing-Fuselage Configuration at a Mach Number of 15.4 and Comparison with Theory,” NASA TN D-3046, 1965, pp. 1–46.
5. AIAA Educational Series;Anderson J. D.,2000