Showing 1 - 20 results of 11,958 for search '(((ping OR (sspinal OR jaina)) OR five) OR (((spans OR (pings OR wings)) OR pin) OR like))', query time: 0.12s Refine Results
  1. 1

    Drag analysis of an aircraft wing model and without bird feather like winglet by Hossain, Altab, Rahman, Mohammed Ataur, Iqbal, A.K.M. Parvez, Ariffin, Muhidin, M., Mazian

    Published 2012
    “…The model of the rectangular wing with bird feather like winglet has been fabricated using polystyrene before design using CATIA P3 V5R13 software and finally fabricated in wood. …”
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    Article
  2. 2

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

    Published 2010
    “…Results reveals a noticeable inboard shift of wing loading for deflected spoiler numbers 5 and 6 at 30o and 40o with jumps in the span load distribution as an indication for the strength of individual vortices (wing/flap vortices). …”
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    Proceeding Paper
  3. 3

    Minimal spanning tree for 100 companies in Bursa Malaysia by Bahaludin, Hafizah, Abdullah, Mimi Hafizah, Mat Salleh, Supian

    Published 2015
    “…This paper investigates the stock market network among the stocks traded in Bursa Malaysia by using minimal spanning tree (MST) techniques. The daily closing prices from 2011 until 2013 of 100 companies based on market capitalization are chosen to construct the network. …”
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    Article
  4. 4

    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
  5. 5

    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
  6. 6

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

    Published 2011
    “…Particle image velocimetry was used in a low-speed wind tunnel to investigate the vortex structures of a slender reverse delta wing at various angles of attack and roll. This work investigates the characteristics of the vortices generated downstream in planes perpendicular to the freestream direction and their dependence on angles of attack and roll at a chord-based Reynolds number of Rec= 382000 The peak tangential velocities at�angle of attack higher than 5 deg show a trend similar to a 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
  11. 11

    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
  12. 12

    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
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    Experience, skill and competence: boundary spanning capabilities for leadership and management of transnational education by Messenger, Hazel, Bloisi, Wendy

    Published 2020
    “…Keywords: activity theory; boundary spanning distributed leadership; partnerships; professional learning community; transnational education…”
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    Book Section
  17. 17

    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
  18. 18

    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
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    5.5-10.5 GHz IR-UWB Pulse Generator for Narrowband Interference Mitigation by Ahmed R., Mohammed, Khalid A. S., Al-Khateeb, Islam, Md. Rafiqul

    Published 2012
    “…An impulse radio ultra wideband (IR-UWB) pulse generator works between 5.5-10.5 GHz for narrowband interference mitigation is proposed. …”
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    Proceeding Paper