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    Scramjet Isolator Shock-Train Leading-Edge Position Modeling Based on Equilibrium Manifold 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 002
    Author(s): Jichao Hu; Juntao Chang; Bin Qin; Lei Wang; Wen Bao; Jiang Qin
    Publisher: American Society of Civil Engineers
    Abstract: A dynamic model showing the relationship between backpressure and shock-train leading edge (STLE) is necessary in the development of a STLE automatic control algorithm. In this research, a nonlinear dynamic model based on ...
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    Ignition Characteristics of a Liquid-Kerosene-Fueled Scramjet during Air Throttling Combined with a Gas Generator 

    Source: Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 005
    Author(s): Wen Bao; Jichao Hu; Youhai Zong; Qingchun Yang; Juntao Chang; Meng Wu; Daren Yu
    Publisher: American Society of Civil Engineers
    Abstract: The ignition characteristics of a flush wall, liquid-kerosene-fueled scramjet combustor are tested in a directly connected ground test rig. The total temperature and Mach number of the vitiated airflow at the exit of the ...
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    Effect of Fuel Injection Allocation on the Combustion Characteristics of a Cavity-Strut Model Scramjet 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 001
    Author(s): Youhai Zong; Wen Bao; Juntao Chang; Jichao Hu; Qingchun Yang; Jian Song; Meng Wu
    Publisher: American Society of Civil Engineers
    Abstract: The cavity-strut supersonic combustion organization method has been found to improve the combustion performance of ethylene in recent studies. In this work, liquid kerosene combustion experiments have been carried out in ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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