Development and key technology analysis of turbine-based combined cycle engine

被引:0
|
作者
Lin, Weiquan [1 ]
Xu, Hangrui [1 ]
Lan, Xudong [1 ]
机构
[1] Aero Engine Research Center, School of Aerospace Engineering, Tsinghua University, Beijing,100084, China
关键词
D O I
10.16511/j.cnki.qhdxxb.2024.27.024
中图分类号
学科分类号
摘要
引用
收藏
页码:1521 / 1535
相关论文
共 50 条
  • [41] Aerodynamic characteristics of over/under inlet for turbine based combined cycle engine
    Coll. of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China
    Tuijin Jishu/Journal of Propulsion Technology, 2008, 29 (06): : 667 - 672
  • [42] Simulation of Fuel System Temperature Rise in Turbine Based Combined Cycle Engine
    Liu Y.-H.
    Li J.-S.
    Tang S.-J.
    Lu D.-Y.
    Dong H.-B.
    Liu, You-Hong (liuyh@buaa.edu.cn), 1600, Journal of Propulsion Technology (41): : 984 - 991
  • [43] Thermo-environmental Analysis of Recuperated Gas Turbine-Based Cogeneration Power Plant Cycle
    Kumari, Anupam
    Sanjay
    ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING, 2016, 41 (02) : 691 - 709
  • [44] Fluid-Structure Interaction Study of the Splitter Plate in Turbine-Based Combined-Cycle Inlet System
    Qin, Qihao
    Xu, Jinglei
    Guo, Shuai
    JOURNAL OF AEROSPACE ENGINEERING, 2017, 30 (04)
  • [45] Development of Flow and Heat Transfer Coupling Simulation Software for Fuel System of Turbine Based Combined Cycle Engine
    Liu Y.-H.
    Zhao X.-W.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (03):
  • [46] An Investigation of Multi-Fidelity Coupling Simulation of over/ under Turbine-Based Combined-Cycle Propulsion System
    Liu J.
    Yuan H.-C.
    Zhang J.-S.
    Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (01): : 21 - 29
  • [47] Probabilistic risk assessment (PRA) approach for the Next Generation Launch Technology (NGLT) Program Turbine-Based Combined Cycle (TBCC) Architecture 6 launch vehicle
    Packard, MH
    Zampino, EJ
    ANNUAL RELIABILITY AND MAINTAINABILITY SYMPOSIUM, 2004 PROCEEDINGS, 2004, : 604 - 609
  • [48] Analysis of mode transition with thrust smoothing of small turbine/ramjet combined cycle engine
    Huang, Hong-Chao
    Wang, Zhan-Xue
    Cai, Yuan-Hu
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (12): : 2756 - 2762
  • [49] Investigation of the impact of splitter rotation speed on mode transition characteristics of an over-under turbine-based combined cycle inlet
    Chen, Liang
    Zhang, Yue
    Xu, Yi-Xuan
    Tan, Hui-Jun
    Xue, Hong-Chao
    Wang, Zi-Yun
    PHYSICS OF FLUIDS, 2024, 36 (08)
  • [50] Review on the aerodynamic issues of the exhaust system for scramjet and turbine based combined cycle engine
    Lv, Zheng
    Xu, Jinglei
    Song, Guangtao
    Li, Rui
    Ge, Jianhui
    PROGRESS IN AEROSPACE SCIENCES, 2023, 143