Showing 61 - 80 results of 192 for search '((((sping OR wing) OR sspinggk) OR jingya) OR (((sspinga OR ssshinga) OR ssspinna) OR pin))', query time: 0.07s Refine Results
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  16. 76

    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
  17. 77

    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
  18. 78

    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
  19. 79

    Bio-fuel-contaminated lubricant and hardening effects on the friction and wear of AISI 1045 steel by Maleque, Md. Abdul, Masjuki, H.H., Ishak, M.

    Published 1998
    “…A study has been made on the wear and fiction of hardened AISI 1045 steel using a pi-pin-ondisc type of fiction and wear apparatus. During the investigation the linear pin wear, coe@cient of friction and rise in pin specimen temperature were monitored and wear and fiction curues 'plotted. …”
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    Article
  20. 80

    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