Showing 41 - 60 results of 1,414 for search '(((spina OR (spinel OR spinel)) OR (skine OR spin)) OR (((pingn OR wings) OR pin) OR link))', query time: 0.09s Refine Results
  1. 41

    Characteristics of treated bamboo/cotton blend yarn produced from ring and rotor spinning techniques by Nor Anuwar, Anis Amirah

    Published 2023
    “…The process of making 50:50 treated bamboo/cotton yarn involved several steps, including opening, carding, rotor spinning, and ring spinning. Treatment type 3 produced the most promising fibre for yarn production, with a fineness of 11.2 tex and tenacity of 12.6 cN/tex, resulting in a spinnable 50:50 treated bamboo/cotton yarn. …”
    Get full text
    Get full text
    Get full text
    Thesis
  2. 42

    Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV) by Omar, Ashraf Ali, Kurban, Adel, Baharuddin, Khairun Nisaa, Ibrahim, Idasary

    Published 2010
    “…This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. …”
    Get full text
    Proceeding Paper
  3. 43

    Effect of angle of incidence on roll damping derivatives of a delta wing by Crasta, Asha, Khan, Sher Afghan

    Published 2014
    “…In the Present paper effect of angle of incidence on roll damping derivative of a delta wing with curved leading edges with attached shock case has been studied. …”
    Get full text
    Article
  4. 44
  5. 45

    Feasibility of QKD over FSO Link by Husagić-Selman, Alma, Al-Khateeb, Wajdi Fawzi Mohammed, Saharudin, Shuhairi

    Published 2012
    “…QKD is possible over fiber cable and Free Space Optical (FSO) links. Fiber based QKD may be used if direct line of sight link is not possible, but it brings along many problems related to material properties of fiber cable and detector limitations. …”
    Get full text
    Proceeding Paper
  6. 46
  7. 47
  8. 48

    The structural and optical properties of Poly(Triarylamine) (PTAA) thin films prepared at defferent spin coating method by Miandal, Kellie, Hoh, Hang Tak, Mohamad, Khairul Anuar, Fuei, Pien Chee, Alias, Afishah

    Published 2017
    “…A series of PTAA thin films were deposited at 1000 rpm to 3000 rpm on a glass substrate by spin coating. The structural and optical properties of the organic p-type semiconductor Poly (triarylamine) at the different spin rate were investigated. …”
    Article
  9. 49

    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. …”
    Get full text
    Article
  10. 50

    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. …”
    Get full text
    Get full text
    Proceeding Paper
  11. 51

    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. …”
    Get full text
    Article
  12. 52

    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. …”
    Get full text
    Article
  13. 53

    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.…”
    Get full text
    Get full text
    Get full text
    Thesis
  14. 54

    Development of duststorm attenuation model for microwave links by Islam, Md. Rafiqul, Khalifa, Othman Omran, Al-Khateeb, Khalid A. Saeed, Elabdin, Zain, Elsheikh, Elfatih A. A.

    Published 2010
    “…Measurements at existing microwave links show that the duststorms can potentially result in serious attenuation in signal level especially at Ku band and higher frequencies with direct impact on telecommunications system performance. …”
    Get full text
    Proceeding Paper
  15. 55
  16. 56
  17. 57
  18. 58

    Effects of kenaf/polyester blending ratios on physical and mechanical properties of yarns produced from ring spinning system by Mohd Rusli, Najwa Wajihah

    Published 2019
    “…This study observed on properties of kenaf/polyester hybrid yarns with different composition of kenaf that was spun using ring spinning system. The development of sliver was prepared by using carding process, the sliver was then inserted into ring spinning machine to produce hybrid yarns. …”
    Get full text
    Get full text
    Get full text
    Thesis
  19. 59

    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.…”
    Get full text
    Proceeding Paper
  20. 60

    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. …”
    Get full text
    Article