1–20 von 136 Ergebnissen
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    Configurations analysis for high-altitude/long-endurance airships

    Yu, Daren / Lv, Xiaowu | Emerald Group Publishing | 2010

    Hysteresis phenomenon of hypersonic inlet at high Mach number

    Jiao, Xiaoliang / Chang, Juntao / Wang, Zhongqi et al. | Elsevier | 2016

    Backpressure propagation mode and balance property in a rectangular duct

    He, Yubao / Huang, Hongyan / Yu, Daren | SAGE Publications | 2019

    Mechanism of shock train rapid motion induced by variation of attack angle

    Xu, Kejing / Chang, Juntao / Zhou, Weixing et al. | Elsevier | 2017

    Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel

    Jiao, Xiaoliang / Chang, Juntao / Wang, Zhongqi et al. | Elsevier | 2016

    Thrust noise cause analysis and suppression of a cusped field thruster

    Cui, Kai / Liu, Hui / Jiang, Wenjia et al. | Elsevier | 2020

    Predictor–Corrector Method for Scramjet Inlet Air Mass Flow Rate Measurement

    Jiao, Xiaoliang / Wang, Zhongqi / Yu, Daren | AIAA | 2017

    Recent research progress on unstart mechanism, detection and control of hypersonic inlet

    Chang, Juntao / Li, Nan / Xu, Kejing et al. | Elsevier | 2016

    Adaptive gas path diagnostics using strong tracking filter

    Pu, Xingxing / Liu, Shangming / Jiang, Hongde et al. | SAGE Publications | 2014

    Ideal Heat Release of Supersonic Combustion

    Cui, Tao / Yang, Shengbo / Yu, Daren | AIAA | 2013

    Hydrogen-fueled scramjet cooling system investigation using combustor and regenerative cooling coupled model

    Bao, Wen / Duan, Yanjuan / Zhou, Weixing et al. | SAGE Publications | 2014

    Design of magnetically enhanced hollow cathode micro-thruster: Concept and experimental research

    Liu, Chenguang / Ning, Zhongxi / Zhu, Ximing et al. | Elsevier | 2023