Wind tunnel tests of hypersonic inlets for ramjet modules of ramjet-scramjet combined engine

被引：0
|
作者：
Internal Flow Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [1 ]
机构：
来源：
Hangkong Xuebao | 2007年 / 4卷 / 783-790期
关键词：
8;
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] Sea-Level Static Tests of Rocket-Ramjet Combined Cycle Engine Model
    Tomioka, Sadatake
    Takegoshi, Masao
    Kochi, Toshinori
    Kato, Kanenori
    Saito, Toshihito
    Tani, Kouichiro
    JOURNAL OF PROPULSION AND POWER, 2021, 37 (03) : 381 - 390
  • [22] Computational analysis of an independent ramjet stream in a combined cycle engine
    Bond, RB
    Edwards, JR
    AIAA JOURNAL, 2004, 42 (11) : 2276 - 2283
  • [23] THE USE OF PULSE FACILITIES FOR TESTING SUPERSONIC COMBUSTION RAMJET (SCRAMJET) COMBUSTORS IN SIMULATED HYPERSONIC FLIGHT CONDITIONS
    ORTH, RC
    ERDOS, JI
    NINTH INTERNATIONAL SYMPOSIUM ON AIR BREATHING ENGINES, VOLS 1 AND 2: SYMPOSIUM PAPERS, 1989, : 596 - 604
  • [24] Complex Investigation of Nonstationary Flow with Shock Waves in the Working Path of a Hypersonic Ramjet Engine
    A. N. Ishchenko
    E. A. Maslov
    N. P. Skibina
    V. V. Faraponov
    Journal of Engineering Physics and Thermophysics, 2021, 94 : 450 - 457
  • [25] Study of heat transfer processes in the flowing part of hypersonic air-ramjet engine
    Maslov, Eugene
    Zharova, Irina
    Faraponov, Valery
    Kozlov, Eugene
    Matskevich, Vladislav
    HEAT AND MASS TRANSFER IN THE THERMAL CONTROL SYSTEM OF TECHNICAL AND TECHNOLOGICAL ENERGY EQUIPMENT (HMTTSC-2018), 2018, 194
  • [26] COMPLEX INVESTIGATION OF NONSTATIONARY FLOW WITH SHOCK WAVES IN THE WORKING PATH OF A HYPERSONIC RAMJET ENGINE
    Ishchenko, A. N.
    Maslov, E. A.
    Skibina, N. P.
    Faraponov, V. V.
    JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2021, 94 (02) : 450 - 457
  • [27] Effect of strut schemes on combustion characteristics in innovative combined ramjet engine
    Zhang, Kai
    Qin, Fei
    Yu, Xuanfei
    Zhu, Shaohua
    Zhang, Duo
    ACTA ASTRONAUTICA, 2024, 222 : 359 - 374
  • [28] INVESTIGATION OF AERODYNAMIC FORCES ON SCRAMJET INLETS USING SHOCK TUNNEL TESTS
    ITO, T
    YAMAZAKI, T
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1995, 38 (121) : 183 - 195
  • [29] Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/ scramjet mode
    Li, Menglei
    Sun, Mingbo
    Li, Peibo
    Yang, Daoning
    An, Bin
    Yao, Yizhi
    Chen, Jikai
    Wang, Taiyu
    Wang, Jiaoru
    CHINESE JOURNAL OF AERONAUTICS, 2024, 37 (03) : 104 - 115
  • [30] Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode
    Menglei LI
    Mingbo SUN
    Peibo LI
    Daoning YANG
    Bin AN
    Yizhi YAO
    Jikai CHEN
    Taiyu WANG
    Jiaoru WANG
    Chinese Journal of Aeronautics, 2024, 37 (03) : 104 - 115
12345