WANG Yuan-guang,XU Xu,CAI Guo-biao.Analysis of design calculation methods of scramjet combustion chamber[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31(1):69-73.(in Chinese)
LU Xi-yun,YANG Guo-wei,ZHUANG Li-xian.Nonlinear dynamic stability analysis for the aircraft flying at high angles of attack[J].Acta Aerodyanica Sinica,1999,17(2):177-182.(in Chinese)
LI Jian-ping,SONG Wen-yan,XIAO Yin-li.Research on the optimization design of integrated scramjet/airframe[J].Journal of Aerospace Power,2011,26(4):874-879.(in Chinese)
[11]
SHAPIRO A H.The dynamics and thermodynamics of compressible fluid flow[M].New York:John Wiley and Sons,1953.
[12]
BREWER K M.Exergy methods for the mission-level analysis and optimization of generic hypersonic vehicles[D].Virgina,USA:Virginia Polytechnic Institute and State Univer-sity,2006.
[13]
CARLSON J R.Prediction of very high Reynolds number compressible skin priction.AIAA 1 998-2 880[R].1998.
[14]
HAZELTON D M,BOWERSOX R D W.Skin friction corrlelations for high enthalpy flows.AIAA 1 998-1 636[R].1998.
WANG Lan,XING Jian-wen,ZHENG Zhong-hua,et al.One-dimensional evaluation of the scramjet flowpath performance[J].Journal of Propulsion Technology,2008,29(6):641-645.(in Chinese)
LIU Ling,LIU Jing-hua,ZHANG Bang,et al.Supersonic combustion and supersonic combustion ramjet engine[M].Xi’an:Northwestern Polytechnical University Press,1993.(in Chinese)
[19]
TAHA A A,TIWARI S N,MOHIELDIN T O.Effect of combustor configuration on the flame holding in scramjet.AIAA 2 003-3 544[R].2003.
ZHAO Zhi,SONG Wen-yan,CAO Yu-ji.Numerical simulation of flow fields in a scramjet combustor with two steps[J].Journal of Changchun University of Science and Technology,2006,29(1):105-108.(in Chinese)