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.…”
Get full text

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. …”
Get full text

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. …”
Get full text

Idea dan pendekatan seni bina melayu moden dalam kalangan arkitek Malaysia by Sabil, Azmal

“…Pengadaptasian nilai rekabentuk seni bina Melayu tradisional kepada bangunan moden telah diwartakan sebagai salah satu jalan di dalam membina bahasa identiti seni bina kebangsaan seperti yang telah dinyatakan di dalam ‘Seminar Ke Arah Identiti Kebangsaan Dalam Seni Bina’ pada tahun 1981. …”
Get full text

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. …”
Get full text

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. …”
Get full text

Amalan keselamatan pengurusan tapak bina oleh majikan pekerja di dalam industri pembinaan by Ali, Roszaidi

Get full text
Get full text

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. …”
Get full text

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. …”
Get full text
Get full text

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. …”
Get full text

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. …”
Get full text

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.…”
Get full text
Get full text
Get full text

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.…”
Get full text

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. …”
Get full text

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. …”
Get full text
Get full text

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. …”
Get full text

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. …”
Get full text
Get full text

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. …”
Get full text

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. …”
Get full text

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. …”
Get full text