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  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. …”
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    Article
  2. 22

    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
  3. 23

    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
  4. 24

    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
  5. 25

    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
  6. 26

    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.…”
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    Proceeding Paper
  7. 27

    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
  8. 28
  9. 29

    Snake-like soft robot using 2-chambers actuator by Abdulrab, Hakim Q.A., Mohd Nordin, Ili Najaa Aimi, Muhammad Razif, Muhammad Rusydi, Faudzi, Ahmad Athif

    Published 2018
    “…Many researchers have been working on snake-like robots due to their flexibility, safety and dexterity. …”
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    Article
  10. 30

    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
  11. 31

    Effect of angle of incidence on roll damping derivatives of a delta wing by Crasta, Asha, Khan, Sher Afghan

    Published 2014
    “…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. …”
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    Article
  12. 32

    The competing interactions on a Cayley tree-like lattice: pentagonal chandelier by Uguz, Selman, Ganikhodjaev, Nasir, Akin, Hasan, Temir, Seyit

    Published 2012
    “…. � = �1) using a generalization of the Cayley tree-like lattice approximation. We study the phase diagrams for the Ising model on a Cayley tree-like lattice, a new lattice type called pentagonal chandelier, with competing nearest- -neighbor interactions J1, prolonged next-nearest-neighbor interactions Jp and one-level next-nearest-neighbor senary interactions J(6)l1 . …”
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    Article
  13. 33

    Tree-like queries in OWL 2 QL: succinctness and complexity results by Bienvenu, Meghyn, Kikot, Stanislav, Podolskii, Vladimir

    Published 2015
    “…Our first contribution is to clarify the worst-case size of positive existential (PE), non-recursive Datalog (NDL), and first-order (FO) rewritings for various classes of tree-like conjunctive queries, ranging from linear queries to bounded treewidth queries. …”
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    Article
  14. 34

    Ammonia detection in water with balloon-like plastic optical fiber sensor by Che Abd Rashid, Nurfatihah, Cholan, Noran Azizan Cholan, Kim Gaik Tay, Kim Gaik Tay, Mat Daud, Azra Munirah, Jaharudin, Nurul Atika Nabila, Sulaiman, Nazrah Ilyana, Ngajikin, Nor Hafizah

    Published 2023
    “…The sensor head is formed by bending an unclad fiber optic sensor into a balloon-like structure. The bending radius of the balloon-like bent fiber optic sensor is varied from 1.0 to 2.5 cm. …”
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    Article
  15. 35
  16. 36

    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

    Published 2013
    “…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. …”
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    Proceeding Paper
  17. 37

    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

    Published 2016
    “…Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. …”
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    Article
  18. 38

    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
  19. 39

    Stability derivatives of a delta wing with straight leading edge in the Newtonian limit by Crasta, Asha, Khan, Sher Afghan

    Published 2013
    “…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. …”
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    Article
  20. 40

    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