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

“…A Strip theory is used in which strips at different span wise location are independent of each other. …”
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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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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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Stability derivatives of a delta wing with straight leading edge in the Newtonian limit by Crasta, Asha, Khan, Sher Afghan

“…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. …”
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The development of a fixed wing aircraft analysis and design flight dynamic software by Ahmad Alaian, Ahmad Eshtiwey

“…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.…”
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A hybrid technique using minimal spanning tree and analytic hierarchical process to prioritize functional requirements for parallel software development by Muhammad Yaseen, Muhammad Yaseen, Mustapha, Aida, Shah, Muhammad Arif, Ibrahim, Noraini

“…This research proposes a hybrid prioritization technique of minimal spanning trees (MST) and AHP called the spanning analytic hierarchical process (SAHP) for FRs prioritization by exploiting MST capability to prioritize large size software FRs with smaller pairwise comparisons but with more consistent results. …”
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A hybrid technique using minimal spanning tree and analytic hierarchical process to prioritize functional requirements for parallel software development by Muhammad Yaseen, Muhammad Yaseen, Mustapha, Aida, Shah, Muhammad Arif, Ibrahim, Noraini

“…This research proposes a hybrid prioritization technique of minimal spanning trees (MST) and AHP called the spanning analytic hierarchical process (SAHP) for FRs prioritization by exploiting MST capability to prioritize large size software FRs with smaller pairwise comparisons but with more consistent results. …”
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A hybrid technique using minimal spanning tree and analytic hierarchical process to prioritize functional requirements for parallel software development by Muhammad Yaseen, Muhammad Yaseen, Mustapha, Aida, Muhammad Arif Shah, Muhammad Arif Shah, Ibrahim, Noraini

“…This research proposes a hybrid prioritization technique of minimal spanning trees (MST) and AHP called the spanning analytic hierarchical process (SAHP) for FRs prioritization by exploiting MST capability to prioritize large size software FRs with smaller pairwise comparisons but with more consistent results. …”
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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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