| Citation: | Simulation of windmilling-ram mode performance for tandem TBCC engine[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.014
|
| [1] |
MCNELIS N,BARTOLOTTA.Revolutionary turbine accelerator (RTA) demonstrator［R］.AIAA-2005-3250,2005.
|
| [2] |
LEDERER R,SCHWAB R,VOSS N.Hypersonic airbreathing propulsion activities for SNGER［R］.AIAA 91-5040,1991.
|
| [3] |
SOSOUNOV V A,TSKHOVREBOV M M,SOLONIN V I,et al.The study of experimental turboramjets［R］.AIAA 92-3720,1992.
|
| [4] |
MIYAGI H,KIMURA H,KISHI K,et al.Combined cycle engine research in Japanese HYPR program［R］.AIAA 98-3278,1998.
|
| [5] |
BLEVINS G,HARTSEL J,POWELL T.Variable concepts for high Mach applications［R］.AIAA 87-2103,1987.
|
| [6] |
刘增文.高超声速飞行器/涡轮基组合循环发动机一体化设计研究［D］.西安:西北工业大学,2010.LIU Zengwen.Integrated design of turbine based combined cycle engine and hypersonic vehicle［D］.Xian:Northwestern Polytechnical University,2010.(in Chinese)
|
| [7] |
何时慧,吴国钏,华清.涡扇发动机风车特性计算［J］.航空发动机,1997,23(3):1-9.
|
| [8] |
李少伟,王如根,吴培根.风车状态静子角度调节对高负荷风扇性能的影响［J］.空军工程大学学报,2013,14(4):19-23.LI Shaowei,WANG Rugen,WU Peigen.Research on effect of stator setting angle adjustment on the highly loaded fan performance during windmilling［J］.Journal of Air Force Engineering University,2013,14(4):19-23.(in Chinese)
|
| [9] |
黄红超,王占学,蔡元虎.基于推力连续准则的小型涡轮冲压组合发动机模态转换过程分析［J］.航空动力学报,2010,25(12):2756-2762.HUANG Hongchao,WANG Zhanxue,CAI Yuanhu.Analysis of mode transition with thrust smoothing of small turbine/ramjet combined cycle engine［J］.Journal of Aerospace Power,2010,25(12):2756-2762.(in Chinese)
|
| [10] |
CHEN M,TANG H L,ZHU Z L.Goal programming for stable mode transition in tandem turbo-ramjet engines［J］.Chinese Journal of Aeronautics,2009,22(5):486-492.
|
| [11] |
MIYAGI H,MIYAGAWA H,MONJI T,et al.Combined cycle engine research in Japanese HYPR project［R］.AIAA 95-2751,1995.
|
| [12] |
KONDO M,MORII S,MURASHIMA K.Overview of the Japanese national project “super/hyper-sonic transport propulsion system program”［R］.AIAA 95-2445,1995.
|
| [13] |
YANAGI R,MORITA M,WATANABE Y,et al.Conceptual design of turbo-accelerator for HST combined cycle engine［R］.ASME Paper 92-GT-253,1992.
|
| [14] |
ITAHARA H,KOHARA S,TAKAGI S,et al.Turbo engine research in Japanese HYPR project for HST combined cycle engines［R］.AIAA 94-3358,1994.
|
| [15] |
SUZUKI M,KUNO N,TOBITA A,et al.Current status of fan component research in HYPR program［R］.AIAA 98-3280,1998.
|
| [16] |
KAWANO M,KUYAMA T,KOBAYASHI M,et al.Development of a high temperature combustor for HYPR Mach 3 turbojet engines［R］.AIAA 98-3281,1998.
|
| [17] |
SHIMIZU K,NOGAMI R.Current status of low pressure turbine component research in HYPR program［R］.AIAA 98-3282,1998.
|
| [18] |
KUO S C,DOERNBACH J D,CHAMPAGNE G,et al.A scoping study for hypersonic transport propulsion systems［R］.ASME Paper 92-GT-409,1992.
|
| [19] |
WALSH P P,FLETCHER P.Gas turbine performance［M］.2nd.Oxford,UK:Blackwell Science ltd,2004.
|
| [20] |
KURZKE J.How to get component maps for aircraft gas turbine performance calculations［R］.ASME Paper 96-GT-164,1996.
|
| [21] |
REIGLER C,BAUER M,KURZKE J.Some aspects of modeling compressor behavior in gas turbine performance calculations［J］.Journal of Turbomachinery,2001,123(2):372-378.
|
| [22] |
王宇,刘建勋,李应红,等.基于抛物线外推的压气机低转速特性研究［J］.航空动力学报,2009,24(5):1136-1142.WANG Yu,LIU Jianxun,LI Yinghong,et al.Research on low speed characteristics of compressor based on parabola extrapolation［J］.Journal of Aerospace Power,2009,24(5):1136-1142.(in Chinese)
|
| [23] |
SEXTON W R.A method to control turbofan engine starting by varying compressor surge valve bleed［D］.Blacksburg,Virginia:The Virginia Polytechnic Institute and State University,2001.
|
| [24] |
GAUDET S R,GAUTHIER D.A simple sub-idle component map extrapolation method［R］.ASME Paper GT2007-27193,2007.
|
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