Low power and high voltage swing cascode Pierce oscillator for MEMS SAW resonators by Md Hamzah, Mohd Haidar, Nordin, Anis Nurashikin, Karim, Jamilah

“…This circuit was designed using Silterra's 0.13um CMOS process and has low power consumption of 1.52mW with high voltage swing 0.10V to 0.99V. All simulations were conducted using Cadence Design Systems. …”
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Robust PID anti-swing control of automatic gantry crane based on Kharitonov's stability by Solihin, Mahmud Iwan, Martono, Wahyudi, Legowo, Ari, Akmeliawati, Rini

“…In this paper, a stable robust PID controller for anti-swing control of automatic gantry crane is proposed. …”
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Intradural extramedullary spinal schwannoma : early surgical outcome of 4 cases by Khan, Ed Simor, Zakaria@Mohamad, Zamzuri, Sharifudin, Mohd Ariff, Ayeop, Mohd Adham Shah, Awang, Mohamed Saufi, Chan, Kin Hup, Seliman, Arfahiza

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Para refah ve huzur getirir mi? (Can money bring prosperity and peace?) by Kayadibi, Saim

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Development of a wireless current controlled stimulator for individuals with spinal cord injury by Masdar, Aizan

“…A spinal cord injury (SCI) has a severe impact on human life in general as well as on the physical status and condition. …”
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Experimental investigation of plain- and flapped-wing tip vortices by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf A., Kwon, Kijung, Jung, Hyejin

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

“…In this work, the IIUM first free wing unmanned aerial vehicle model (IIUM-FWUAV) was investigated experimentally. …”
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Development of educational software for stress analysis of an aircraft wing by Mohamed Ali, Jaafar Syed, Sadeq, Tazkera

“…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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Flow visualization over a circular planform wing by Suliman , M. M. Ali, Omar, Ashraf Ali, Syed Mohamed Ali, Jaffar

“…circular plan form wing at high Reynolds numbers has been carried out numerically. …”
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Oscillating supersonic delta wings with curved leading edges by Khan, Sher Afghan, Crasta , Asha

“…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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Effect of angle of incidence on stability derivatives of a wing by Crasta, Asha, Khan, Sher Afghan

“…In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. …”
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Oscillating supersonic delta wing with straight leading edges by Crasta, Asha, Khan, Sher Afghan

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

“…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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Evaluation of aircraft wing-tip vortex using PIV by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali

“…The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. …”
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Book Review, Military Legal Proceedings in Malaysia: Teo Say Eng & Colonel Wan Nor Mazlan (2009), LexisNexis(HardCover) by Ab Aziz, Shamrahayu

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Right-wing nationalism, populism, and religion: what are the connections and why? by Haynes, Jeffrey

“…This collection focuses on right-wing nationalism, populism, and religion, both theoretically and empirically, with an emphasis on the following countries: Australia, India, Italy, Turkey, and the USA. …”
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Continuous spinal anesthesia for lower limb surgery in patient with poor left ventricular function by Mohamed, Rozilah @ Abdul Hadi, Md Ralib, Azrina, Lukman, Mohd Fahmi, Abdullah, Nor Zamzila, Osman, Ariff, Mat Nor, Mohd Basri

“…Continuous spinal anaesthesia (CSA) has been found to produce good haemodynamic control and prolongation of anaesthetic and analgesic. …”
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Posterolateral lumbar spinal fusion in the New Zealand white rabbit model: surgical techniques by Buyong, Zunariah, Zakaria@Mohamad, Zamzuri, Khalid, Kamarul Ariffin, Zulkifly, Ahmad Hafiz, Abdel Wahab, Emad Mohamad Nafie

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Induced rolling moment for NACA4412 plain and flapped wing by Elsayed, Omer Ali, Kwon, Kijung, Asrar, Waqar, Omar, Ashraf Ali E.

“…Purpose – The paper aims to compute rolling moments on a follower aircraft wing due to vortices generated by a plain and flapped NACA4412 wing using experimental particle image velocimetery (PIV) data. …”
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Investigation of the vortical flow around a reverse delta wing by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar, Ludin@Jamaluddin, Hani

“…A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing.…”
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