Attacks on Shen et. al.’s remote user authentication scheme and defense* by Pathan, Al-Sakib Khan, Hong, Choong Seon

“…We show various types of forgery attacks against Shen et. al.’s timestamp-based scheme and improve their scheme to ensure robust security for the remote authentication process keeping almost all the advantages that were present in their scheme. …”
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Using affinity set on finding the key attributes of delayed diagnosis by Larbani, Moussa, Chen, Yuh-Wen, Chen, Chao-Wen, Shen, Chih-Min

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Numerical investigation of the vortical flow over delta wing and reverse delta wing by Omar, Ashraf Ali E., Jamaluddin, Hani Ludin, Asrar, Waqar

“…This study aims to give some thoughts and initial understanding of passive wake vortex alleviation by introducing add-ons devices onto the aircraft, which are delta wing (DW) and reverse delta wing (RDW). However, as a preliminary investigation, the study has treated these devices separately from the aircraft in order to clearly visualize the wake vortex formation behind the wing as a standalone. …”
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Optimum length for pin fins used in electronic cooling by Mafeed, M. P., M., Salman Ali, C., Prabin, Ramis, M. K., Ali Baig, M. A., Khan, Sher Afghan

“…The present work deals with the heat transfer analysis of pin fins of various geometries namely ─ circular, triangular and rectangular and thus arrive at the optimum design. …”
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Study of the reverse delta wing by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar

“…A six-component balance was used to obtain the aerodynamic coefficients for a reverse delta wing as well as a delta wing for comparison. A simulation of the streamlines, velocity vectors, and surface pressure contours was carried out using computational fluid dynamics software to show the characteristics of the flow over a reverse delta wing.…”
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Pinning for judges in harmonising Civil Law and Shariah: Challenges and prospects by Shuaib, Farid Sufian

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Experimental investigation of wing tip vortex by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung, Jung, Hyejin

“…Particle image velocimetery was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a SWIM model was used as a vortex generator in two different configurations, (i) plain wing and (ii) flapped wing with trailing edge flap extended at 20 degrees. …”
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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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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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Pin type reconfigurable clamping ability evaluation for setup-free technology by Afzeri, Afzeri, Sutjipto, Agus Geter Edy, Nurul Amin, A.K.M

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An experimental study on precision grinding of silicon using diamond grinding pins by Alao, Abdur-Rasheed, Konneh, Mohamed

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Autonomous goal finding robot by Kamal, M. A. S., Khan, Md. Raisuddin, -, Faisal, Billah, Md. Masum

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Flutter analysis of supersonic wing with external stores by Abdullah, Nur Azam, Sulaeman, Erwin

“…In the present paper, the simulation of supersonic wing equipped with external loads of missiles on the wing had been analyzed at high supersonic region. …”
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Right-wing populism and religion in Europe and the USA by Haynes, Jeffrey

“…The aim of this paper is to examine comparatively the growth and political effectiveness of right-wing populism in Western Europe, Central Europe, and the USA since 9/11. …”
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Analysis of Dijkstra’s and A* algorithm to find the shortest path by Alija, Amani Saleh

“…There are so many algorithms used to find the shortest path such as Dijkstra, A* algorithm, Genetic algorithm, Floyd algorithm and Ant algorithm. …”
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Evaluation of aircraft wing-tip vortex using PIV by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali

“…Particle image velocimetry was used in a wind tunnel to measure the tip vortex velocity field and hence investigate the flow structure in a wake of aircraft half-wing model. The purpose of this investigation is to evaluate the main features of the lift generated vortices in order to find ways to alleviate hazardous wake vortex encounters for follower airplanes during start and approach such that the increase in airport capacity can be achieved. …”
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Internet banking in Pakistan: finding complexities by Akhlaq, Mohammed ather, Shah, Asadullah

“…Out of the nine complexities identified, six are found significant. The findings of the research signify that 67 % of the proposed complexities, Familiarity with the technology, Concerns for Download Speed, Unfriendly Website Design, Fear of Government tracking transactions, Security and People Gaining Access/Misusing, hinder the users in accepting and adopting internet banking technology in Pakistan.…”
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Proceedings of the Seminar on Research Findings 2008

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Finding and funding voices: the London experience by Lewis, Peter M.

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Fact-finding missions : the Strasbourg experience by Paraskeva, Costas

“…However, where fundamental facts remain in dispute between the parties, the ECtHR has, in the past, conducted fact-finding missions. The basis upon which such fact-finding missions are conducted is to be found in Art. 38(1) ECHR which provides simply that the Court may, "if need be, undertake an investigation". …”
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