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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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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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

“…Posterior element of T12 and bilateral erector spinae muscles sent for histopathological evaluation. …”
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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

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

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

“…This article discusses the relationship between good governance and the administrative corruption. It outlines the findings and results that have been done among public servants. …”
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Experiences of struggle : findings from a longitudinal study by Leathwood, Carole

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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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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

“…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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