Effect of base contour on aerospike nozzle performance

被引：0
|
作者：
Dai, Wu-Ye
Liu, Yu
Zhang, Zheng-Ke
机构：
来源：
Yuhang Xuebao/Journal of Astronautics | 2002年 / 23卷 / 02期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [21] Experimental analysis of jet flow in an aerospike nozzle
    Alshiya, K. Sankari Ashok
    Santhosh, M.
    Santhosh, V. K.
    Gopal, S. Sai
    MATERIALS TODAY-PROCEEDINGS, 2021, 46 : 3444 - 3450
  • [22] Design and Optimization of Aerospike nozzle using CFD
    Kumar, Naveen K.
    Gopalsamy, M.
    Antony, Daniel
    Krishnaraj, R.
    Viswanadh, Chaparala B. V.
    1ST INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN AEROSPACE ENGINEERING (ICRAAE-2017), 2017, 247
  • [23] Numerical analysis of the clustered type aerospike nozzle flow: Flow structures and thrust performance
    Ito, T
    Fujii, K
    COMPUTATIONAL FLUID DYNAMICS 2002, 2003, : 285 - 290
  • [24] SWIRLING FLOW EFFECTS ON THE AEROACOUSTIC SIGNATURE OF AN AEROSPIKE NOZZLE
    Golliard, Thomas
    Mihaescu, Mihai
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12C, 2024,
  • [25] Design and optimization of aerospike nozzle for rotating detonation engine
    Liu, Xiang-Yang
    Cheng, Miao
    Zhang, Yun-Zhen
    Wang, Jian-Ping
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 120
  • [26] Regression study of scramjet nozzle performance on contour parameters
    Zhang, W.-D., 1600, Beijing University of Aeronautics and Astronautics (BUAA) (28):
  • [27] BASIC FLOW CHARACTERISTICS OF A LINEAR AEROSPIKE NOZZLE SEGMENT
    MUELLER, TJ
    SULE, WP
    MECHANICAL ENGINEERING, 1973, 95 (04) : 59 - 59
  • [28] Designing an axisymmetric aerospike nozzle based on modified MOC
    Masdari, M.
    Tahani, M.
    Fard, F. Mohammadi
    SCIENTIA IRANICA, 2019, 26 (02) : 834 - 842
  • [29] Simulated tests and data acquisition system for aerospike nozzle
    Dai, Wu-Ye
    Liu, Yu
    Cheng, Xian-Chen
    Tuijin Jishu/Journal of Propulsion Technology, 2000, 21 (04): : 85 - 88
  • [30] Numerical analysis of slipstream effect influence on aerospike performance
    Li, J.
    Guo, T.W.
    Ma, J.H.
    2001, China Spaceflight Society (22):
12345