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    Tip Clearance Investigation of a Ducted Fan Used in VTOL Unmanned Aerial Vehicles—Part II: Novel Treatments Via Computational Design and Their Experimental Verification 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 002:;page 21005
    Author(s): Akturk, Ali; Camci, Cengiz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ducted fan based vertical lift systems are excellent candidates to be in the group of the next generation vertical lift vehicles, with many potential applications in general aviation and military missions. Although ducted ...
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    Tip Clearance Investigation of a Ducted Fan Used in VTOL Unmanned Aerial Vehicles—Part I: Baseline Experiments and Computational Validation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 002:;page 21004
    Author(s): Akturk, Ali; Camci, Cengiz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ducted fans that are popular choices in vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAV) offer a higher static thrust/power ratio for a given diameter than open propellers. Although ducted fans provide ...
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    Factors Influencing Computational Predictability of Aerodynamic Losses in a Turbine Nozzle Guide Vane Flow 

    Source: Journal of Fluids Engineering:;2016:;volume( 138 ):;issue: 005:;page 51103
    Author(s): Turgut, أ–zhan H.; Camci, Cengiz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with the computational predictability of aerodynamic losses in a turbine nozzle guide vane (NGV) flow. The paper shows that threedimensional (3D) computations of ReynoldsAveraged Navier Stokes (RANS) ...
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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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