[1] 乐嘉陵. 吸气式高超声速技术研究进展[J]. 推进技术, 2010, 31(6): 641-649. (LE Jia-ling. Progress in Air-Breathing Hypersonic Technology[J]. Journal of Propulsion Technology, 2010, 31(6): 641-649.)
[2] 刘兴洲. 中国超燃冲压发动机研究回顾[J]. 推进技术, 2008, 29(4): 385-394. ( LIU Xing-zhou. Review of Scramjet Research in China[J]. Journal of Propulsion Technology, 2008, 29(4): 385-394.)
[3] 杨凯, 原志超, 朱强华, 等. 高超声速热化学非平衡钝体绕流数值模拟[J]. 推进技术, 2014, 35(12): 1585-1591. (YANG Kai, YUAN Zhi-chao, ZHU Qiang-hua, et al. Numerical Simulation of Hypersonic Thermochemical Nonequiliburium Blunt Body Flows[J].Journal of Propulsion Technology, 2014, 35(12): 1585-1591.)
[4] 刘健, 原志超, 杨凯, 等. 高超声速飞行器多层复杂热防护结构气-固耦合快速热分析方法[J]. 推进技术, 2016, 37(2): 227-234. (LIU Jian, YUAN Zhi-chao, YANG Kai, et al. Fast Algorithm of Coupled Flow-Thermal for Multi-Layered Complex TPS of Hypersonic Aircraft[J]. Journal of Propulsion Technology, 2016, 37(2): 227-234.)
[5] Le Jialing. Preliminary Study of Integrated Aero-Propulsive Performance of Vehicle with CFD and Experiments[R]. AIAA 2006-7982.
[6] Li Mailiang, Zhou Jin, GengHui, et al. Investigations on Function of Cavity in Supersonic Combustion Using OH PLIF[R]. AIAA 2004-3657.
[7] Tumino G, Mancuso S, Gallego J-M, et al. The IXV Experience, from the Mission Conception to the Flight Results[J]. Acta Astronautica, 2016, 124: 2-17.
[8] Roberto Angelini, Angelo Denaro. IXV Re-Entry Demonstrator: Mission Overview, System Challenges and Flight Reward[J]. Acta Astronautica, 2016, 124: 18-30.
[9] Klaus Hannemann. Hypersonic Flight and Re-Entry in Germany-Overview and Selected Projects[C]. San Fancisco: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2011.
[10] Javier Bartolome Calvo, Thino Eggers. Application of a Coupling of Aerodynamics and Flight Dynamics to the SHEFEX I Flight Experiment[R]. AIAA 2011-2323.
[11] John Turner, Marcus H?rschgen, Josef Ettl, et al. SHEFEX 2 Development Status of the Vehicle and Sub-Systems for a Hypersonic Re-Entry Flight Experiment[C]. Bad Reichenhall: 19th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2009.
[12] The SHEFEX Team. SHEFEX II 2nd Flight within DLR’s Re-Entry Technology and Flight Test Program[EB/OL]. www.esaconferencebureau.com/docs/default-source/projectcode-docs/shefex-II-2nd -flight-within-dir’s-re-entry-technology-and-flight-test-program.pdf, 2016-08-01.
[13] JBarrio A M, Sudars M, Aulisio R, et al. EXPERT: The ESA Experimental Re-Entry Test-Bed[R]. AIAA 2011-6342.
[14] Massobrio F, Viotto R, Serpicob M, et al. EXPERT: An Atmospheric Re-Entry Test-Bed[J]. Acta Astronautica, 2007, 60: 974-985.
[15] Ottens H, Walpot L. Aerodynamic Environment and Flight Measurement Techniques of EXPERT[R]. AIAA 2006-8118.
[16] The Spaceflight101 Team. IXV-Intermediate Experimental Vehicle[EB/OL]. www.spacelight101.com/spacecraft/ixv-intermediate-experimental-vehicle.pdf, 2016-08-01.
[17] Ali Gülhan, Thomas Thiele, Frank Siebe. Challenges of the Instrumentation for High Speed Entry Vehicles[EB/OL]. www.solarsystem.nasa.gov/docs/2-Guelhan-Instrumentation.pdf, 2016-08-01.
[18] Francesca Cipollini, Jean-Marie Muylaert. European Activities on Advanced Flight Measurement Techniques for Hypersonic Space Vehicles[R]. AIAA 2006-3832.
[19] Herdrich G, L?hle S, Auweter-Kurtz M, et al. IRS Ground-Testing Facilities: Thermal Protection System Development, Code Validation and Flight Experiment Development[R]. AIAA 2004-2596.
[20] Muylaert J, Cipollini F, Walpot L, et al. Flight Experiments for Hypersonic Vehicle Development Expert[R]. ESA/RTO-EN-AVT-116, 2004. * 收稿日期:2017-10-02；修订日期:2017-12-06。作者简介:张云昊,女,硕士,高级工程师,研究领域为特种试验与测量技术。E-mail: yunhaO2004@sina.com(编辑:朱立影)
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