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    Comparison Analysis between Expander Cycle and Recooling Cycle for a Scramjet 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    Author(s): Jiang Qin; Wen Bao; Weixing Zhou
    Publisher: American Society of Civil Engineers
    Abstract: An expander cycle is one potential fuel feeding cycle for a scramjet, which has been successfully applied in the liquid rocket. However, very little literature exists about the fuel feeding cycle for a scramjet. A recooling ...
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    The Impact of Surface Drag on the Structure and Evolution of Surface Boundaries Associated with Tornadogenesis in Simulated Supercells 

    Source: Monthly Weather Review:;2023:;volume( 151 ):;issue: 012:;page 3037
    Author(s): Jiang, Qin; Dawson, Daniel T.
    Publisher: American Meteorological Society
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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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    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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