Prevalence of elevated aldosterone renin ratio in three main states of Peninsular Malaysia by Saud Gany, Siti Liyana, Shahar, Mohammad Arif, Sukor, Norlela, Omar, Ahmad Marzuki, A Wahab, Norasyikin, MY, Yusniza, Azizan, Elena, Chong, Kuck Meng, Md Zain, Rabizah, Long, Kha Ching, Mohd Razali, Amyliation, Zainuddin, Noradilah, Mat, Nurul Hani, Mender, Fadlin, Muhair, Musilawati, Othman, Hanita, Yusof, Siti Fatehah, Rahmat, Norhisham, Saufi, Ahmad, Bador, Khalidah Mazlan, Kamaruddin, Nor Azmi

“…Only 7 (5.9%) of them were hypokalemic, one of them being hypertensive. The main clinical characteristics of subjects with raised ARR are shown in Table 1. …”
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Back pain and osteolysis of the thoracic spine in an adult: a case of monostotic fibrous dysplasia masquerading as spinal metastasis by Zakaria@Mohamad, Zamzuri, Sharifudin, Mohd Ariff, Mohamed Amin, Mohamed Azril, Abd. Aziz, Azian, Khan, Ed Simor, Goh, Kian Liang

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Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges by Crasta, Asha, Khan, Sher Afghan

“…In the present study hypersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with curved leading edges for the attached shock case. …”
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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.

“…Findings – Results obtained showed that the maximum induced rolling moment coefficient depends on the strength of the vortex produced by the generating aircraft wing and increases linearly with the increment of the angle of attack. …”
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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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Estimation of stability derivatives of a delta wing in hypersonic flow by Crasta, Asha, Baig, Maugal Ahmed Ali, Khan, Sher Afghan

“…In the present study supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for attached shock case. A strip theory is used in which strips at different span wise locations are independent. …”
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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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Cellular radio based vehicular location finding by Anwar, Farhat

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Exploration to find green building materials from recycled solid wastes by Din, Abdul Talib, Mohd Hafiz, Norzawahir, Mohd Rus, Anika Zafiah

“…This project therefore discussed mainly about theory of heat transfer which consist of conduction and radiation. …”
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Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV) by Omar, Ashraf Ali, Kurban, Adel, Baharuddin, Khairun Nisaa, Ibrahim, Idasary

“…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. …”
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Administrative corruption and good governance in Iraq: finding and analysis by Ismail, Ibrahim, Abbas, Rafid Ali

“…It was found that job satisfaction is the main factor that contributes to the reduction of corruption. …”
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Effect of angle of incidence on roll damping derivatives of a delta wing by Crasta, Asha, Khan, Sher Afghan

“…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. …”
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سونمي : قصص من ماليزيا (Sunami : qasas min Malaziya) by El-Nagar, Hassan Abdelrazig

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Malamih min al-Bayan An-Nabawiy: Dirasah Ta'siliyyah by Mansour, Saad eldin

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İslam Birliği: Orta yolu bulmak (Islamic Unity: To find the Middle Way) by Kayadibi, Saim

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Experiences of struggle : findings from a longitudinal study by Leathwood, Carole

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Main causes of civilian vulnerability in a non- international armed conflict: An appraisal of the legal factors by Hamid, Abdul Ghafur@Khin Maung Sein

“…There may be legal as well as non-legal factors that are the main causes of the civilian harm in a non-international armed conflict. …”
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A study of the legal effect of the main provisions of the income tax treaty between France and the United Kingdom by McKee, Sophie A. Hoquet

“…This thesis analyses the taxation rules applicable to different classes of income and the respective rights to tax of both the state of source and the state of residence. Its main objective is to provide an exhaustive explanation of the rules of taxation, together with an illustration of their practical operation. …”
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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

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

“…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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