Showing 1 - 20 results of 822 for search '(((pina OR ping) OR shen) OR (((scans OR ((pingk OR lingk) OR wings)) OR ssspinga) OR eng))', query time: 0.13s Refine Results
  1. 1

    Spiral scanning: an alternative to conventional raster scanning in high-speed Scanning Probe Microscopes by Mahmood, Iskandar Al-Thani, Moheimani, S.O. Reza

    Published 2010
    “…A spiral scanning method for high-speed Atomic Force Microscopy (AFM) is described in this paper. …”
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    Proceeding Paper
  2. 2

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

    Published 2006
    “…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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    Proceeding Paper
  3. 3

    Study of the reverse delta wing by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar

    Published 2011
    “…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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    Article
  4. 4

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

    Published 2009
    “…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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    Proceeding Paper
  5. 5

    Right-wing populism and religion in Europe and the USA by Haynes, Jeffrey

    Published 2020
    “…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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    Article
  6. 6

    Fast spiral-scan atomic force microscopy by Mahmood, Iskandar Al-Thani, Moheimani, S.O. Reza

    Published 2009
    “…In this paper, we describe a new scanning technique for fast atomic force microscopy. …”
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    Article
  7. 7

    Experimental investigation of plain- and flapped-wing tip vortices by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf A., Kwon, Kijung, Jung, Hyejin

    Published 2009
    “…Particle image velocimetry was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a subsonic wall interference model was used as a vortex generator in two different configurations: 1) plain wing and 2) flapped wing with the trailing-edge flap extended at 20 degrees. …”
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    Article
  8. 8

    Experimental investigation of free wing IIUM-UAV configuration by Omar, Ashraf Ali, Mohd Yusof, Mohammad Fairuzi, Mohd Sani, Mohd Afnan

    Published 2010
    “…In this work, the IIUM first free wing unmanned aerial vehicle model (IIUM-FWUAV) was investigated experimentally. …”
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    Proceeding Paper
  9. 9

    Evaluation of aircraft wing-tip vortex using PIV by Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali

    Published 2009
    “…The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. …”
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    Proceeding Paper
  10. 10
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  12. 12

    Induced rolling moment for NACA4412 plain and flapped wing by Elsayed, Omer Ali, Kwon, Kijung, Asrar, Waqar, Omar, Ashraf Ali E.

    Published 2010
    “…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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    Article
  13. 13

    Investigation of the vortical flow around a reverse delta wing by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar, Ludin@Jamaluddin, Hani

    Published 2011
    “…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
    Proceeding Paper
  14. 14

    Right-wing nationalism, populism, and religion: what are the connections and why? by Haynes, Jeffrey

    Published 2021
    “…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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    Article
  15. 15

    Using affinity set on mining the necessity of computed tomography scanning by Chen , Yuh Wen, Larbani, Moussa, Li, Tzung Hung, Chen, Chao-Wen

    Published 2009
    “…In this study, the trauma patients, who were treated by the CT scanning are collected in order to discover the critical knowledge; that is, what characteristics of trauma patients would lead to the necessity of CT scanning? …”
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    Article
  16. 16

    A new scanning method for fast atomic force microscopy by Mahmood, Iskandar Al-Thani, Moheimani, S.O. Reza, Bhikkaji, Bharath

    Published 2011
    “…In this paper, we describe a new scanning method for fast atomic force microscopy. In this technique, the sample is scanned in a spiral pattern instead of the well-established raster pattern. …”
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    Article
  17. 17

    Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV) by Omar, Ashraf Ali, Kurban, Adel, Baharuddin, Khairun Nisaa, Ibrahim, Idasary

    Published 2010
    “…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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    Proceeding Paper
  18. 18
  19. 19

    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

    Published 2012
    “…This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. …”
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    Article
  20. 20

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

    Published 2016
    “…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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    Thesis