Showing 21 - 40 results of 11,958 for search '(((ping OR (sspinal OR jaina)) OR five) OR (((spans OR (pings OR wings)) OR pin) OR like))', query time: 0.13s Refine Results
  1. 21

    Oscillating supersonic delta wing with straight leading edges by Crasta, Asha, Khan, Sher Afghan

    Published 2012
    “…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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    Article
  2. 22

    Effect of angle of incidence on stability derivatives of a wing by Crasta, Asha, Khan, Sher Afghan

    Published 2014
    “…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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    Article
  3. 23

    Development of educational software for stress analysis of an aircraft wing by Mohamed Ali, Jaafar Syed, Sadeq, Tazkera

    Published 2012
    “…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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    Article
  4. 24

    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
  5. 25

    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
  6. 26

    Flow visualization over a circular planform wing by Suliman , M. M. Ali, Omar, Ashraf Ali, Syed Mohamed Ali, Jaffar

    Published 2013
    “…circular plan form wing at high Reynolds numbers has been carried out numerically. …”
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    Proceeding Paper
  7. 27

    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
  8. 28

    iKool ointment - 10% eucalyptus oil, 5% peppermint oil, 5% menthol, 5% camphor by Mohamed, Farahidah, Chatterjee, Bappaditya, Ahmad, Kausar

    Published 2020
    “…Label displaying the brand name iKool and main ingredients i.e 10% eucalyptus oil, 5% peppermint oil, 5% menthol, 5% camphor in ointment bases, with other instruction and labeling as required by regulatory.…”
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    Copyright
  9. 29

    Pembangunan kerangka strategi dalam penyelesaian harta tanah Al-Mafqud di Malaysia by Sulaiman, Muhammad Azwan

    Published 2017
    Subjects: “…HD50-50.5 Delegation of authority. Decentralization. Span of control…”
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    Thesis
  10. 30

    How to cope with dengue in the developing countries like Pakistan? by Sohail, Filza, Alam, Gazi Mahabubul, Khan, Rizwan Rasul, Naeem, Rahmah

    Published 2011
    “…A viral disease like dengue lacking a specific form of treatment is a high menace to human health. …”
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    Article
  11. 31

    Untitled (Group of five men) by Wexford Association, WA

    “…Black and white photograph showing five men wearing suits and hats, one wearing two rosettes. …”
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    Photograph
  12. 32

    Group portrait of five men by Waterford Association, WA

    “…Black and white group portrait photograph of five men. Photographer unknown.…”
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    Photograph
  13. 33
  14. 34

    Firearm recognition based on whole firing pin impression image via backpropagation neural network by Ahmad Kamaruddin, Saadi, Md Ghani, Nor Azura, Liong, Choong-Yeun, Jemain, Abdul Aziz

    Published 2011
    “…In this study, a set of data which focused on selected 6 features of firing pin impression images before an entirety of five different pistols of South African made; the Parabellum Vector SPI 9mm model, were used. …”
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    Book Chapter
  15. 35

    Firearm recognition based on whole firing pin impression image via backpropagation neural network by Ahmad Kamaruddin, Saadi, Md Ghani, Nor Azura, Liong, Choong-Yeun, Jemain, Abdul Aziz

    Published 2011
    “…In this study, a set of data which focused on selected 6 features of firing pin impression images before an entirety of five different pistols of South African made; the Parabellum Vector SPI 9mm model, were used. …”
    Get full text
    Proceeding Paper
  16. 36

    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
  17. 37

    Frequency reconfiguration mechanism of a PIN diode on a reconfigurable antenna for LTE and WLAN Applications by Mohd Shah, Shaharil, Daud, M. F. M., Zainal Abidin, Zuhairiah, Che Seman, Fauziahanim, Hamzah, Shipun Anuar, Katiran, Norshidah

    Published 2018
    “…In this work, a frequency reconfigurable antenna with a BAR63-02V Positive-Intrinsic-Negative (PIN) diode is designed, simulated and fabricated. …”
    Article
  18. 38
  19. 39

    Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges by Crasta, Asha, Khan, Sher Afghan

    Published 2012
    “…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. …”
    Get full text
    Article
  20. 40

    Estimation of stability derivatives of a delta wing in hypersonic flow by Crasta, Asha, Baig, Maugal Ahmed Ali, Khan, Sher Afghan

    Published 2012
    “…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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    Article