郭峰 , 朱剑锋 , 尤延铖 , 邢菲 . 涡轮基组合动力与火箭的耦合特性分析及匹配优化设计[J]. 航空学报, 2021 , 42(7) : 124755 -124755 . DOI: 10.7527/S1000-6893.2020.24755

[1] 左光,艾邦成. 先进空间运输系统气动设计综述[J]. 航空学报, 2021, 42(2):624077. ZUO G, AI B C.Aerodynamic design of advanced space transportation system:Review[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(2):624077(in Chinese).
[2] HUETER U, MCCLINTON C, COOK S. NASA's advanced space transportation hypersonic program:AIAA-2002-5175[R]. Reston:AIAA, 2002.
[3] 刘君, 袁化成, 葛宁. 串联式TBCC进气道模态转换模拟器设计及其特性分析[J]. 航空学报, 2016, 37(12):3675-3684. LIU J, YUAN H C, GE N. Design and flow characteristics analysis of mode transition simulator for tandem type TBCC inlet[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(12):3675-3684(in Chinese).
[4] BULMAN M, SIEBENHAAR A. Combined cycle propulsion:Aerojet innovations for practical hypersonic vehicles[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2011.
[5] GUO F, LUO W G, GUI F, et al. Efficiency analysis and integrated design of rocket-augmented turbine-based combined cycle engines with trajectory optimization[J]. Energies, 2020, 13(11):2911.
[6] SIEBENHAAR A, BOGAR T. Integration and vehicle performance assessment of the aerojet "TriJet" combined-cycle engine[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2009.
[7] WEI B X, LING W H, LUO F T, et al. Propulsion performance research and status of TRRE engine experiment[C]//21 st AIAA International Space Planes and Hypersonics Technologies Conference. Reston:AIAA, 2017.
[8] 郭峰, 桂丰, 尤延铖, 等. 一种涡轮基组合动力的整机低速风洞试验研究[J]. 推进技术, 2019, 40(11):2436-2443. GUO F, GUI F, YOU Y C, et al. Experimental study of TBCC engine performance in low speed wind tunnel[J]. Journal of Propulsion Technology, 2019, 40(11):2436-2443(in Chinese).
[9] SERRE L, DEFOORT S. LAPCAT Ⅱ:Towards a Mach 8 civil aircraft concept, using advanced Rocket/Dual-mode ramjet propulsion system[C]//16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2009.
[10] BENSON T, TREFNY C, WALKER J, et al. Interactive design tool for turbine based combined cycle engines[C]//33rd Joint Propulsion Conference and Exhibit. Reston:AIAA, 1997.
[11] CLOUGH J. Modeling and optimization of turbine based combined cycle engine performance[D]. College Park:University of Maryland, 2004.
[12] DANIEL A H, ERIC J G. Integrated turbine-based combined cycle dynamic simulation model:E-17775P[R]. Washington, D.C.:NASA, 2011.
[13] 张冬青, 宋文艳, 柴政, 等. 组合循环发动机飞机/发动机性能一体化分析[J]. 航空动力学报, 2017, 32(10):2498-2508. ZHANG D Q, SONG W Y, CHAI Z, et al. Aircraft/engine performance integrated analysis on combined cycle engine[J]. Journal of Aerospace Power, 2017, 32(10):2498-2508(in Chinese).
[14] 韦宝禧, 凌文辉, 冮强, 等. TRRE发动机关键技术分析及推进性能探索研究[J]. 推进技术, 2017, 38(2):298-305. WEI B X, LING W H, GANG Q, et al. Analysis of key technologies and propulsion performance research of TRRE engine[J]. Journal of Propulsion Technology, 2017, 38(2):298-305(in Chinese).
[15] 江晨钟. TBCC推进系统与飞行器耦合建模及特性分析[D]. 哈尔滨:哈尔滨工业大学, 2017:29-49. JIANG C Z. The coupled modeling and characteristics analysis of TBCC propulsion system and aerocraft[D]. Harbin:Harbin Institute of Technology, 2017:29-49(in Chinese).
[16] 张明阳, 王占学, 刘增文, 等. Ma4一级内并联式TBCC发动机模态转换性能分析[J]. 推进技术, 2017, 38(2):315-322. ZHANG M Y, WANG Z X, LIU Z W, et al. Analysis of mode transition performance for a Mach 4 over-under TBCC engine[J]. Journal of Propulsion Technology, 2017, 38(2):315-322(in Chinese).
[17] 宋自航, 唐海龙, 陈敏. 高超声速并联TBCC总体性能分析与模态转换仿真[J]. 航空发动机, 2019, 45(1):33-39. SONG Z H, TANG H L, CHEN M. Overall performance analysis and modal conversion simulation of hypersonic parallel TBCC[J]. Aeroengine, 2019, 45(1):33-39(in Chinese).
[18] BENSON D, HUNTINGTON G, THORVALDSEN T, et al. Direct trajectory optimization and costate estimation via an orthogonal collocation method[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston:AIAA, 2006.
[19] ROSS I M. A roadmap for optimal control:The right way to commute[J]. Annals of the New York Academy of Sciences, 2005, 1065(1):210-231.
[20] 杜昕, 李海阳, 沈红新. 基于路径约束分析的跳跃式再入轨迹优化[J]. 航空学报, 2014, 35(5):1265-1275. DU X, LI H Y, SHEN H X. Skip reentry trajectory optimization based on analysis of path constraints[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(5):1265-1275(in Chinese).
[21] BRYSON A E, DESAI M N, HOFFMAN W C. Energy-state approximation in performance optimization of supersonic aircraft[J]. Journal of Aircraft, 1969, 6(6):481-488.
[22] PARKER J T, SERRANI A, YURKOVICH S, et al. Control-oriented modeling of an air-breathing hypersonic vehicle[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(3):856-869.
[23] BROCK M A. Performance study of two-stage-to-orbit reusable launch vehicle propulsion alternatives[D]. Wright-Patterson Air Force Base:Air Force Institute of Technology, 2004.
[24] ZHENG J L, CHANG J T, YANG S B, et al. Trajectory optimization for a TBCC-powered supersonic vehicle with transition thrust pinch[J]. Aerospace Science and Technology, 2019, 84:214-222.
[25] 程荣辉, 张志舒, 陈仲光. 第四代战斗机动力技术特征和实现途径[J]. 航空学报, 2019, 40(3):022698. CHENG R H, ZHANG Z S, CHEN Z G. Technical characteristics and implementation of the fourth-generation jet fighter engines[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(3):022698(in Chinese).
[26] 李乐, 姜光泰, 褚显应, 等. TBCC飞行器发动机尺寸选型及爬升策略设计[J]. 宇航学报, 2018, 39(1):17-26. LI Y, JIANG G T, CHU X Y, et al. Research on TBCC engine size selection and ascent strategy of combined-cycle aircraft[J]. Journal of Astronautics, 2018, 39(1):17-26(in Chinese).
[27] DARBY C L, HAGER W W, RAO A V. An hp-adaptive pseudospectral method for solving optimal control problems[J]. Optimal Control Applications and Methods, 2011, 32(4):476-502.
[28] HEISER W H, PRATT D T. Hypersonic airbreathing propulsion[M]. 5th ed. Reston:AIAA, 1994:114-116.
[29] RAYMER D P. Aircraft design:A conceptual approach[M]. 4th ed. Reston:AIAA, 1992:460-461.