Showing 41 - 60 results of 2,052 for search '(((pin OR yong) OR ming) OR ((((pink OR (ping OR wings)) OR shing) OR minga) OR (min OR line)))', query time: 0.12s Refine Results
  1. 41

    Palmprint recognition using principal lines characterization by Rotinwa-Akinbile, M. O., Aibinu, Abiodun Musa, Salami, Momoh Jimoh Emiyoka

    Published 2011
    “…In this paper, a novel contactless Palmprint recognition system using palm print principal line-based feature extraction technique has been proposed. …”
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    Proceeding Paper
  2. 42

    Dielectric measurement based microstrip transmission line by Ikhsan, Fatin Hamimah

    Published 2019
    “…A microstrip line having impedance other than 50 Ω is designed and material under test is used as the substrate. …”
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    Thesis
  3. 43

    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
    “…This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. …”
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    Article
  4. 44

    Numerical simulation of a low aspect ratio wing at low Reynolds number by Suliman , M. M. Ali, Omar, Ashraf Ali, Syed Mohamed Ali, Jaffar, M. Syuhairi |, M. Husain

    Published 2013
    “…In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. …”
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    Proceeding Paper
  5. 45

    Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft by UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Ali, JS Mohamed

    Published 2016
    “…Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. …”
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    Article
  6. 46

    Stability derivatives of a delta wing with straight leading edge 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
  7. 47

    The development of a fixed wing aircraft analysis and design flight dynamic software by Ahmad Alaian, Ahmad Eshtiwey

    Published 2016
    “…Through the implementation of five types of aircraft models, the developed computer code represents a useful tool for flight dynamic analysis and control design for a fixed-wing aircraft.…”
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    Thesis
  8. 48
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    Tuning fork UWB antenna with unsymmetrical feed line by Alam, A. H. M. Zahirul, Islam, Md. Rafiqul, Khan, Sheroz

    Published 2012
    “…A simple planar rectangular UWB is designed with unsymmetrical feed line. It is observed that the unsymmetrical feed line plays an important role for increasing the antenna bandwidth. …”
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    Proceeding Paper
  11. 51

    Noise Emissions Mapping from Ampang Line LRT by Arbaan, A, Othman, M H, Tong, Y G, Ab Ghani, A R, Ambak, K, Borhan, M N, Abdul Sukor, N S

    Published 2023
    “…The aims of this study are to evaluate Light Rail Transit (LRT) noise level in urban area, at LRT Ampang Line by using grid lines method and to develop LRT noise mapping. …”
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    Conference or Workshop Item
  12. 52

    Classification of critical aging segments of power transmission lines by Mohamed Ariffin, Nur Azliatun Hisan

    Published 2011
    “…The thermal ratings of power transmission lines is basically based on the maximum permissible temperature of the conductors. …”
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    Thesis
  13. 53

    Printing fine solid lines in flexographic printing process by Yusof, Mohd Sallehuddin

    Published 2011
    “…Solid lines are essential to enable printing of conducting tracks for various electronic applications. …”
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    Thesis
  14. 54

    Experimental investigation of the vortical flow around a reverse delta wing using PIV by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar

    Published 2010
    “…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 a plane perpendicular to the free stream direction and their dependence on angles of attack and roll angles at chord based Reynolds number.…”
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    Proceeding Paper
  15. 55

    Prediction of energy absorption capability of curved panel structure; for wing leading edge study by Omar, Norihan, Md Khalid, Nur Aisyah, Shamsudin, Nor Fadilah, Aminanda, Yulfian

    Published 2012
    “…This paper works on the curvature effect of wing leading edge structure subjected to impact loading. …”
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    Article
  16. 56

    Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure by Omar, Nurihan, Aminanda, Yulfian, Syed Mohamed Ali, Jaffar

    Published 2014
    “…This paper works on the curvature composite structure for wing leading edge application using fabric carbon/epoxy material subjected to impact loading. …”
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    Article
  17. 57

    Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow by Crasta, Asha, Khan, Sher Afghan

    Published 2016
    “…In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. …”
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    Article
  18. 58

    The Fixed wing UAV usage on land use mapping for gazetted royal land in Malaysia by Hj. Mohd. Noor, Norzailawati, Harun, Nor Zalina, Abdullah, Alias

    Published 2020
    “…The study deals with the usage of fixed wing unmanned aerial vehicle (UAV) in verifying boundary for gazetted royal land, which the other sight of efficacy of UAV has been tested in area of urban planning. …”
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    Proceeding Paper
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