Showing 61 - 80 results of 192 for search '(((pinn OR spingaool) OR (wing OR ssspinee)) OR (((wing OR pinga) OR spings) OR pin))', query time: 0.06s Refine Results
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  15. 75

    Evolution of NACA23012 wake vortices structure using PIV by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung

    Published 2012
    “…The formation and development of a wing‐tip vortex in a near and extended near field were studied experimentally. …”
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    Article
  16. 76

    Design of a planar structure of multifrequency patch antenna by Alam, A. H. M. Zahirul, Islam, Md. Rafiqul, Khan, Sheroz

    Published 2008
    “…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. The effect of gap between driven patch and the wing patches have been studied for multiband frequency operation. …”
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    Article
  17. 77

    Span load modification via differential spoiler setting by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali

    Published 2010
    “…The serious impact of the wing tips vortices of a large aircraft is well known. …”
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    Proceeding Paper
  18. 78

    Stabilty derivatives in the newtonian limit by Crasta, Asha, Khan, Sher Afghan

    Published 2013
    “…They are applicable for wings of arbitrary plan form shape at high angles of attack provided the shock wave is attached to the leading edge of the wing. …”
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    Article
  19. 79

    Investigation of Empennage Location Effect to the Unmanned Aerial Vehicle (UAV) Structure Characteristic by Norazman, Farid Dania, Ariffin, Ahmad Hamdan, Firman Sahifulddin, Mohd Rahmat, Abdul Ranini, lrfan

    Published 2024
    “…Interestingly, the hybridization of fixed-wing and rotary UAV gives better performance in terms of energy consumption and the needs of runaway. …”
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    Article
  20. 80

    Investigation of aerodynamic parameters of a hybrid airship by Andan, Amelda Dianne, Asrar, Waqar, Omar, Ashraf Ali

    Published 2012
    “…The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. …”
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    Article