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    Effects of Flow Distortions as They Occur in S Duct Inlets on the Performance and Stability of a Jet Engine 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 002:;page 22605
    Author(s): Rademakers, Rudolf. P. M.; Bindl, Stefan; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One of the research areas at the Institute of Jet Propulsion focuses on the design and optimization of sshaped engine inlet configurations. The distortion being evoked within such inlet ducts should be limited to ensure ...
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    On Intake–Compressor Interactions Within an Integrated Propulsion System 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 005:;page 51012-1
    Author(s): Rademakers, Rudolf. P. M.; Stößel, Marcel; Kožulović, Dragan; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The integration of a propulsion system into the airframe can contribute to the overall aircraft performance and is beneficial for military applications due to a reduction of the aircraft radar cross section. On the other ...
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian