Protection of human rights and the environment: links and approaches by Abdulkadir, A.B., Mustafa, Maizatun, Ansari, Abdul Haseeb

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Fade dynamics analysis for for terrestrial microwave links by Zyoud, Al-Hareth, Dao, Hassan, Islam, Md. Rafiqul, Chebil, Jalel, Al-Khateeb, Khalid A. Saeed, Abd Rahman, Tharek

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Poverty link to the environment: international and national perspectives by Ansari, Abdul Haseeb

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

“…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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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

“…This paper works on the curvature effect of wing leading edge structure subjected to impact loading. …”
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Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure by Omar, Nurihan, Aminanda, Yulfian, Syed Mohamed Ali, Jaffar

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

“…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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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

“…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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Government linked companies: The impact of GLCs transformation policy by Ab. Rashid, Hafiz Majdi

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Rain rate distribution for microwave link design in Malaysia by Chebil, Jalel, Abd Rahman, Tharek

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Performance evaluation of Free-Space-Optic (FSO) links by Alma, Husagic, Al-Khateeb, Wajdi Fawzi Mohammed

“…Knowing the losses or attenuation within the channel it is then possible to evaluate received power level and link margin, the main figures needed in order to evaluate the performance ofFSO links…”
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Rain attenuation prediction models for earth-space link by Ismail, Ahmad Fadzil, Badron, Khairayu

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Parameterized indoor propagation model for mobile communication links by Zyoud, Al-Hareth, Habaebi, Mohamed Hadi, Islam, Md Rafiqul

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Performance metrics for the prediction of link and path availability in VANETs by Muhammed Yusof, Zulkefli, Flint, James A.

“…The method described makes use of the concept of link availability estimates which are produced on an individual link basis and which may be combined by multiplication to produce a quality metric for the whole route. …”
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Reward management: linking employee motivation and organizational performance by Antoni, Conny H., Baeten, Xavier, Perkins, Stephen J., Shaw, Jason D., Vartiainen, Matti

“…They also illustrate the need to understand the underlying mediating and moderating mechanisms linking reward systems and practices to individual, team, and organizational behavior and outcomes. …”
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An improved functional link neural network for data classification by Iqbal, Umer

“…Accordingly, two alternative models namely; Genocchi Functional Link Neural Network (GFLNN) and Chebyshev Wavelets Functional Link Neural Network (CWFLNN) are proposed. …”
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Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV) by Omar, Ashraf Ali E., Kurban, Adel

“…In this work, IIUM’s first free wing unmanned aerial vehicle model (IIUM-FWUAV) was designed, fabricated, tested and investigated experimentally. …”
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Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow by Ghosh, K, Murthy, M, Khan, Sher Afghan, Pandey, P K

“…Ghosh's unified similitude has been applied to oscillating delta wings of arbitrary plan forms in supersonic/ hyper- sonic flow. …”
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Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges by Crasta, Asha, Khan, Sher Afghan

“…In the Present paper effect of angle of incidence on Stiffness derivative of a delta wing with Curved leading edges for attached shock case in Supersonic Flow has been studied. …”
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Impact of a reverse delta type add-on device on the flap-tip vortex of a wing by Altaf, Afaq, Tan, Boon Thong, Omar, Ashraf Ali, Asrar, Waqar

“…The effect of interactions of vortices produced by an outboard flap-tip of a half-span wing (NACA 23012 in landing configuration) and a slender reverse delta type add-on device, placed in the proximity of the outboard flap-tip, on the upper surface of the half-span wing is investigated using Particle Image Velocimetry in a closed loop low speed wind tunnel. …”
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