Showing 21 - 40 results of 13,304 for search '(((sspina OR esspinar) OR five) OR ((((ching OR than) OR pin) OR (spine OR wing)) OR eng))', query time: 0.13s Refine Results
  1. 21

    Oscillating supersonic delta wings 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. …”
    Get full text
    Article
  2. 22

    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. …”
    Get full text
    Get full text
    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. …”
    Get full text
    Article
  4. 24

    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. …”
    Get full text
    Get full text
    Proceeding Paper
  5. 25

    Oscillating supersonic delta wings with curved leading edges by Khan, Sher Afghan, Crasta , Asha

    Published 2010
    “…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. …”
    Get full text
    Article
  6. 26

    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. …”
    Get full text
    Proceeding Paper
  7. 27

    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.…”
    Get full text
    Get full text
    Copyright
  8. 28
  9. 29

    Book Review, Military Legal Proceedings in Malaysia: Teo Say Eng & Colonel Wan Nor Mazlan (2009), LexisNexis(HardCover) by Ab Aziz, Shamrahayu

    Published 2010
    “…It provides guide for those directly involved in courts-martial proceedings such as the defence counsel and the courts' officers, including the judges of the courts-martial. 4 However, it was suggested in the book review that few matters regarding substance and technical parts of the book should be improved to make it more informative and useful. 5…”
    Get full text
    Article
  10. 30

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

    “…Black and white photograph showing five men wearing suits and hats, one wearing two rosettes. …”
    Get full text
    Photograph
  11. 31

    Group portrait of five men by Waterford Association, WA

    “…Black and white group portrait photograph of five men. Photographer unknown.…”
    Get full text
    Photograph
  12. 32
  13. 33

    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
    Book Chapter
  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. …”
    Get full text
    Proceeding Paper
  15. 35

    Bayatyan v Armenia by Sahakyan, Siranush

    Published 2012
    “…This article discusses the recent landmark judgment in the case of Bayatyan v Armenia (No. 23459/03) 7.07.11 in which the European Court of Human Rights (ECtHR) broke with previous case law and decided to include conscientious objectors within the scope of Art. 9 of the European Convention on Human Rights (ECHR): the right to freedom of thought, conscience and religion.…”
    Get full text
    Article
  16. 36

    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
  17. 37
  18. 38

    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. …”
    Get full text
    Article
  19. 39

    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
  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. …”
    Get full text
    Article