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    The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software

    The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software by Al Aian, Ahmad Eshtiwey

    Published 2011
    “…through series of aerodynamics assessment aircraft components (fuselage, wing, airfoil on the control surface and it's high lift devices). …”
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    Thesis

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