Showing 1,101 - 1,120 results of 5,004 for search '((espinal OR (spinae OR find)) OR ((((sping OR wings) OR shen) OR sspina) OR pin))', query time: 0.07s Refine Results
  1. 1101
  2. 1102

    Untitled (Publicity notice board) by N/A, N/A

    “…Black and white photograph showing three posters pinned to a wall under the sign 'Publicity'. Photographer unknown.…”
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    Photograph
  3. 1103

    Influence of Eu3+ Ions on Elastic Moduli and Microhardness of Zinc‑boro‑soda‑lime‑silica Glass System by Cheong, Wei Mun, Mohd Zaid, Mohd Hafz, Matori, Khamirul Amin, Fen, Yap Wing, Tee, Tan Sin, Loh, Zhi Wei, Mayzan, Mohd Zul Hilmi

    Published 2024
    “…Likewise, the ZBS-3Eu glass sample exhibits the most rigidity attributed to its highest fg value of 0.075. These findings suggest that ZBS-3Eu has the potential for applications requiring high-strength glass.…”
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    Article
  4. 1104
  5. 1105
  6. 1106

    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
  7. 1107
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  11. 1111

    Numerical investigation of the effect of spoiler’s configuration on wake vortex by Omar, Ashraf Ali E., Asrar, Waqar, Ludin @Jamaluddin, Hani

    Published 2012
    “…A numerical investigation was undertaken to study the aerodynamic characteristics of wake vortices generated from an aircraft during taking-off or landing, and thus exploring the possible techniques of reducing hazard imposed to the following aircraft by means of passive wake vortex alleviation by using delta wing (DW) as an add-on device. Simulations were performed using RANS turbulence model.…”
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    Monograph
  12. 1112

    Influence of differential spoiler settings on the wake the vortex characterization and alleviation by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung

    Published 2010
    “…Experimental investigations using particle image velocimetry technique have been carried out for the evaluation of the differential spoiler setting capabilities in modifying the spanwise wing load and further reduce the wake vortex hazard. …”
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    Article
  13. 1113

    Influence of differential spoiler settings on the wake vortex characterization and alleviation by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung

    Published 2010
    “…Experimental investigations using particle image velocimetry technique have been carried out for the evaluation of the differential spoiler setting capabilities in modifying the spanwise wing load and further reduce the wake vortex hazard. …”
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    Article
  14. 1114

    Development of the IIUM hybrid airship by Ping, Julian T.K., Andan, Amelda D., Asrar, Waqar, Omar, Ashraf Ali

    Published 2010
    “…In this paper, the preliminary design steps of a winged hull hybrid airship will be outlined and discussed together with a way to achieve controllability of the hybrid airship during both STOL (Short take off and Landing) and cruising mode as well as its aerodynamic characteristics.…”
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    Proceeding Paper
  15. 1115

    Book review : The people vs. democracy: why our freedom is in danger and how to save it / by Yascha Mounk by Haynes, Jeffrey

    Published 2019
    “…Trump, who he identifies unequivocally as a right-wing populist. If there is one thing guaranteed to make liberal democrats sit up and take notice it is the idea that the United States, for many a venerable bastion of liberal democracy, is now part of a new and highly unexpected populist landscape.…”
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    Article
  16. 1116

    Ballistic impact fracture behaviour of continuous fibre reinforced al-matrix composites by Ali, Al-Hamdan, Nimir, Yassin Lutfi Mahmud, Mustafa, Ramadan J.

    Published 2010
    “…The materials response under high energy impact loads was studied using a gas gun. The projectiles were pins 1.2-1.5 mm in diameter and weighing 0.347-0.435 g. …”
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    Article
  17. 1117
  18. 1118

    Reconfigurable patch antenna by RF MEMS switches by Alam, A. H. M. Zahirul, Islam, Md. Rafiqul

    Published 2009
    “…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. Cantilever MEMS bridges are introduced to provide to operate antenna either 21.73 GHz or 23.6 GHz depending on the position of the MEMS switches. …”
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    Proceeding Paper
  19. 1119

    Reconfigurable patch antenna by RF mems switches by Alam, A. H. M. Zahirul, Islam, Md. Rafiqul

    Published 2009
    “…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. Cantilever MEMS bridges are introduced to provide to operate antenna either 21.73 GHz or 23.6 GHz depending on the position of the MEMS switches. …”
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    Proceeding Paper
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