1Mcnamara J J, Friedmann P P. Aeroelastic and aerother- moelastic analysis in hypersonic flow: past, present, and future. AIAA Journal, 2011, 49(6) : 1089-1122. 被引量:1
2Bertin J J. Hypersonic aerothermodynamics. Reston, VA: AIAA, 1994. 被引量:1
3Dugundji J, Calligeros J M. Similarity laws for aerother- moelastic testing. Journal of Aerospace Sciences, 1962, 29(8) : 935-950. 被引量:1
4Michopoulos J G, Farhat C, Fish J. Survey on modeling and simulation of multiphysics systems, 2005. 被引量:1
6McNamara J J. Aeroelastic and aerothermoelastic behav- ior of two and three dimensional lifting surfaces in hyper- sonic flow. The University of Michigan, 2005. 被引量:1
7Culler A, McNamara J. Coupled flow-thermal-structuralanalysis for response prediction of hypersonic vehicle skin panels. 51 st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2010. 被引量:1
8Ashley H,Zartarian G.Piston theory-a new aerodynamic tool for the aeroelastician[J].Journal of the Aeronautical Sciences,1956,23(12):1109-1118. 被引量:1
9Van Dyke M D.A study of second-order supersonic flow theory[R].Technology Report 1081,NACA,1952. 被引量:1
10Zartarian G,Hsu P T,Ashley H.Dynamic airloads and aeroelastic problems at entry Mach numbers[J].Journal of the Aerospace Sciences,1961,28(3):209-222. 被引量:1