61–80 von 85 Ergebnissen
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    Mathematical Model of Shock-Train Path with Complex Background Waves

    Li, Nan / Chang, Juntao / Yu, Daren et al. | AIAA | 2016

      Mathematical Model of Shock-Train Path with Complex Background Waves

      Li, Nan | Online Contents | 2016
      Beteiligte: Chang, Juntao

      Mathematical Model of Shock-Train Path with Complex Background Waves

      Li, Nan | Online Contents | 2016
      Beteiligte: Chang, Juntao

    Influence Factors of Unstart Boundary for Hypersonic Inlets

    Chang, Juntao / Yu, Daren / Bao, Wen et al. | AIAA | 2008

    Indirect measurement method of inner wall temperature of scramjet with a state observer

    Zhang, Cong / Qin, Jiang / Yang, Qingchun et al. | Elsevier | 2015

      Indirect measurement method of inner wall temperature of scramjet with a state observer

      Zhang, Cong | Online Contents | 2015
      Beteiligte: Chang, Juntao

    Combustion characteristics of a dual-mode scramjet injecting liquid kerosene by multiple struts

    Yang, Qingchun / Bao, Wen / Zong, Youhai et al. | SAGE Publications | 2015

    Comment on “Parametric Ideal Scramjet Cycle Analysis”

    Yang, Qingchun / Chang, Juntao / Zhang, Duo et al. | AIAA | 2014

    Numerical Investigation of Local Resistance to Backpressure in Hypersonic Inlet with Suction

    He, Yubao / Chang, Juntao / Bao, Wen et al. | AIAA | 2016

    Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy

    Cao, Ruifeng / Chang, Juntao / Tang, Jingfeng et al. | Elsevier | 2014

    Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine

    Chang, Juntao / Wang, Lei / Bao, Wen et al. | AIAA | 2014

    Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels

    Wang, Ziao / Xin, Xuanan / Huang, Renzhe et al. | Elsevier | 2022

    Development and evolution mechanism of streamwise vortex in an inward-turning inlet

    Wang, Ziao / Xin, Xuanan / Chen, Ruoyu et al. | SAGE Publications | 2023

    Supersonic Inlet Dynamics Model Based on Equilibrium Manifold

    He, Baocheng / Chang, Juntao / Bao, Wen et al. | AIAA | 2006

    Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet

    Bao, Wen / Zong, Youhai / Chang, Juntao et al. | SAGE Publications | 2014

    New Method for Solving One-Dimensional Transonic Reacting Flows of a Scramjet Combustor

    Cao, Ruifeng / Cui, Tao / Yu, Daren et al. | AIAA | 2016

      New Method for Solving One-Dimensional Transonic Reacting Flows of a Scramjet Combustor

      Cao, Ruifeng | Online Contents | 2016
      Beteiligte: Chang, Juntao

      New Method for Solving One-Dimensional Transonic Reacting Flows of a Scramjet Combustor

      Cao, Ruifeng | Online Contents | 2016
      Beteiligte: Chang, Juntao

    Investigation of hypersonic inlet pulse-starting characteristics at high Mach number

    Jiao, Xiaoliang | Online Contents | 2016
    Beteiligte: Chang, Juntao