Showing 1 - 20 results of 344 for search '(((pinn OR sainal) OR (ssssping OR shinae)) OR (((spent OR (ssping OR ling)) OR wings) OR pin))', query time: 0.10s Refine Results
  1. 1

    Numerical investigation of the vortical flow over delta wing and reverse delta wing by Omar, Ashraf Ali E., Jamaluddin, Hani Ludin, Asrar, Waqar

    Published 2012
    “…This study aims to give some thoughts and initial understanding of passive wake vortex alleviation by introducing add-ons devices onto the aircraft, which are delta wing (DW) and reverse delta wing (RDW). However, as a preliminary investigation, the study has treated these devices separately from the aircraft in order to clearly visualize the wake vortex formation behind the wing as a standalone. …”
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    Proceeding Paper
  2. 2

    Optimum length for pin fins used in electronic cooling by Mafeed, M. P., M., Salman Ali, C., Prabin, Ramis, M. K., Ali Baig, M. A., Khan, Sher Afghan

    Published 2012
    “…The present work deals with the heat transfer analysis of pin fins of various geometries namely ─ circular, triangular and rectangular and thus arrive at the optimum design. …”
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    Article
  3. 3

    Study of the reverse delta wing by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar

    Published 2011
    “…A six-component balance was used to obtain the aerodynamic coefficients for a reverse delta wing as well as a delta wing for comparison. A simulation of the streamlines, velocity vectors, and surface pressure contours was carried out using computational fluid dynamics software to show the characteristics of the flow over a reverse delta wing.…”
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    Article
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    Experimental investigation of wing tip vortex by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung, Jung, Hyejin

    Published 2009
    “…Particle image velocimetery was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a SWIM model was used as a vortex generator in two different configurations, (i) plain wing and (ii) flapped wing with trailing edge flap extended at 20 degrees. …”
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    Proceeding Paper
  7. 7

    Oscillating supersonic delta wings with curved leading edges by Khan, Sher Afghan, Crasta , Asha

    Published 2010
    “…In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. …”
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    Article
  8. 8

    Oscillating supersonic delta wings with straight leading edges by Crasta, Asha, Khan, Sher Afghan

    Published 2012
    “…A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. …”
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    Article
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    Flutter analysis of supersonic wing with external stores by Abdullah, Nur Azam, Sulaeman, Erwin

    Published 2013
    “…In the present paper, the simulation of supersonic wing equipped with external loads of missiles on the wing had been analyzed at high supersonic region. …”
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    Proceeding Paper
  13. 13

    Right-wing populism and religion in Europe and the USA by Haynes, Jeffrey

    Published 2020
    “…The aim of this paper is to examine comparatively the growth and political effectiveness of right-wing populism in Western Europe, Central Europe, and the USA since 9/11. …”
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    Article
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    The Exploration of the Characteristics of Concrete Incorporating Ultrafine Coal Bottom Ash and Spent Garnet by Wan Chik, Wan Muhammad Eddie Khusyairi, Mokhatar, Shahrul Niza, Othman, Nor Hazurina, AAlbshir Budiea, Ahmed Mokhtar, Muthusamy, Khairunisa

    Published 2024
    “…Two such materials, ultrafine coal bottom ash (uCBA) and spent garnet (SG), have shown potential as substitutes for cement and fine aggregate, respectively. …”
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    Article
  17. 17

    The Exploration of the Characteristics of Concrete Incorporating Ultrafine Coal Bottom Ash and Spent Garnet by Wan Chik, Wan Muhammad Eddie Khusyairi, Mokhatar, Shahrul Niza, Othman, Nor Hazurina, Albshir Budiea, Ahmed Mokhtar, Muthusamy, Khairunisa

    Published 2024
    “…Two such materials, ultrafine coal bottom ash (uCBA) and spent garnet (SG), have shown potential as substitutes for cement and fine aggregate, respectively. …”
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    Article
  18. 18

    Experimental investigation of plain- and flapped-wing tip vortices by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf A., Kwon, Kijung, Jung, Hyejin

    Published 2009
    “…Particle image velocimetry was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a subsonic wall interference model was used as a vortex generator in two different configurations: 1) plain wing and 2) flapped wing with the trailing-edge flap extended at 20 degrees. …”
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    Article
  19. 19

    Experimental investigation of free wing IIUM-UAV configuration by Omar, Ashraf Ali, Mohd Yusof, Mohammad Fairuzi, Mohd Sani, Mohd Afnan

    Published 2010
    “…In this work, the IIUM first free wing unmanned aerial vehicle model (IIUM-FWUAV) was investigated experimentally. …”
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    Proceeding Paper
  20. 20

    Development of educational software for stress analysis of an aircraft wing by Mohamed Ali, Jaafar Syed, Sadeq, Tazkera

    Published 2012
    “…The developed software can be used to estimate load on a wing and to compute the stresses at any point along the span of the wing of a given aircraft. …”
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    Article