[1] Chase R L, Boyd D R, Czysz D P, et al. An AJAX technology advanced SSTO design concept, AIAA-1998-5527. Reston: AIAA, 1998.[2] Bityurin V A, Lineberry J T, Litchford R J, et al.Thermodynamic analysis of the AJAX propulsion concept (invited), AIAA-2000-0445. Reston: AIAA, 2000.[3] Sheikin E G, Kuranov A L. Scramjet with MHD bypass under "AJAX" concept, AIAA-2004-1192. Reston: AIAA, 2004.[4] van Wie D M, Nedungadi A. Plasma aerodynamic flow control for hypersonic inlets, AIAA-2004-4129. Reston: AIAA, 2004.[5] Kuranov A, Korabelnikov A. Hypersonic technologies of atmospheric cruise flight under AJAX concept, AIAA-2008-2524. Reston: AIAA, 2008.[6] Li Y W, Li Y H, Zhang B L, et al. Supersonic magnetohydrodynamic technical experimental system based on shock tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(6): 1015-1024. (in Chinese) 李益文, 李应红, 张百灵, 等. 基于激波风洞的超声速磁流体动力技术实验系统[J]. 航空学报, 2011, 32(6): 1015-1024.[7] Zhu T, Li Y H, Zhang B L, et al. Transient acceleration system of magnetoplasmadynamic supersonic airstream and its experimental research[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(8): 1375-1383.(in Chinese) 朱涛, 李应红, 张百灵, 等. 磁激等离子体超声速气流的瞬态加速系统及其实验研究[J]. 航空学报, 2012, 33(8): 1375-1383.[8] Macheret S O, Shneider M N, Miles R B. Electron beam generated plasmas in hypersonic MHD channels, AIAA-1999-3635. Reston: AIAA, 1999.[9] Alderman B, Howard P, Shneider M, et al. Thermionic power conversion for scramjets and reentry vehicles using nanosecond voltage pulses, AIAA-2008-4098.Reston: AIAA, 2008.[10] Udagawa K, Gorbatov S, Pliavaka F, et al. Experimental study of a fast ionization wave discharge at high pulse repetition rates, AIAA-2008-1104. Reston: AIAA, 2008.[11] Murray R C, Zaidi S H, Carraro M R, et al. Magnetohydrodynamic power generation using externally ionized, cold, supersonic air as working fluid[J]. AIAA Journal, 2006, 44(1): 119-127.[12] Nishihara M. Low-temperature supersonic flow control using repetitively pulsed MHD force. Columbus: Department of Mechanical Engineering, The Ohio State University, 2006.[13] Zhukov V P, Kindisheva S V, Kirpichnikov A A, et al, Plasma production for MHD power generation by nanosecond discharge, AIAA-2006-1370. Reston: AIAA, 2006.[14] Udagawa K. Experimental study of a fast ionization wave discharge at high pulse repetition rates, AIAA-2008-1104. Reston: AIAA, 2008.[15] Wu R L, Wang Z Y. Wind tunnel design principle[M]. Beijing: Beijing Aviation College Press, 1985.(in Chinese) 伍荣林, 王振羽. 风洞设计原理[M]. 北京:北京航空学院出版社, 1985.[16] Luo Y H, Ran J X, Wang X X. Comparision study of dielectric barrier discharge in inert gases at atmospheric pressure[J]. High Voltage Engineering, 2012, 38(5): 1070-1077. (in Chinese) 罗云海, 冉俊霞, 王新新. 大气压不同惰性气体介质阻挡放电特性的比较[J]. 高电压技术, 2012, 38(5): 1070-1077.[17] Zhao Q, Liu S Z, Tong H H. Plasma technology and its application[M]. Beijing: National Defense Industry Press, 2009.(in Chinese) 赵青, 刘述章, 童洪辉. 等离子体技术及应用[M]. 北京: 国防工业出版社, 2009.[18] Raizer Y P, Kisin V I, Allen J E. Gas discharge physics[M]. Berlin: Springer-Verlag, 1991. |