Showing 41 - 60 results of 816 for search '(((pinna OR sspinal) OR spinal) OR ((((swing OR wing) OR pink) OR bring) OR (peng OR eng)))', query time: 0.11s Refine Results
  1. 41

    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
  2. 42

    Separation of palm kernel oil from palm kernel with supercritical carbon dioxide using pressure swing technique by Sarker, Md. Zaidul Islam, Nik Ab Rahman, Nik Norulaini, Abdul Kadir, Mohd. Omar, Yoshiyuki, Sato, R. L., Smith Jr.

    Published 2007
    “…The pressurization-depressurization treatments are denoted as pressure swing (PS) extractions. Extractions were performed at 353.2 K and at pressures from 10 to 25 MPa. …”
    Get full text
    Article
  3. 43
  4. 44

    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. …”
    Get full text
    Proceeding Paper
  5. 45

    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. …”
    Get full text
    Article
  6. 46
  7. 47

    Relationship between pulmonary function and the degree of spinal deformity among adolescent idiopathic scoliosis (AIS) patients by Johari, Joehaimey, Nor, Sobri, Lam, Andrew, Omar, Ahmad Sabri, Abdullah, Ahmad Tajudin, Ab Rahman, Azriani, Sharifudin, Mohd Ariff, Yusof, Mohd Imran

    Published 2013
    “…Kruskal-Wallis and Mann Whitney tests were used to compare the lung function according to different levels of affected spinal vertebrae and the severity of the deformity. …”
    Get full text
    Get full text
    Proceeding Paper
  8. 48

    A rare case of monostotic spinal fibrous dysplasia mimicking solitary metastatic lesion of thyroid carcinoma by Sharifudin, Mohd Ariff, Zakaria@Mohamad, Zamzuri, Awang, Mohamed Saufi, Mohamed Amin, Mohamed Azril, Abd. Aziz, Azian

    Published 2016
    “…Magnetic resonance imaging revealed isolated osteolytic lesion over the posterior element of the T12 vertebra with narrowing of the spinal canal causing compression of the cord. The diagnosis of fibrous dysplasia was made histologically. …”
    Get full text
    Get full text
    Article
  9. 49

    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. …”
    Get full text
    Article
  10. 50

    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. …”
    Get full text
    Get full text
    Proceeding Paper
  11. 51

    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. …”
    Get full text
    Article
  12. 52

    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
  13. 53

    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. …”
    Get full text
    Article
  14. 54

    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.…”
    Get full text
    Get full text
    Get full text
    Thesis
  15. 55
  16. 56

    Back pain and osteolysis of the thoracic spine in an adult: a case of monostotic fibrous dysplasia masquerading as spinal metastasis by Zakaria@Mohamad, Zamzuri, Sharifudin, Mohd Ariff, Mohamed Amin, Mohamed Azril, Abd. Aziz, Azian, Khan, Ed Simor, Goh, Kian Liang

    Published 2013
    “…MR imaging revealed isolated osteolytic lesion over posterior element of T12 vertebra with narrowing of the spinal canal causing compression to the cord. CT-guided biopsy did not obtain any malignant cells. …”
    Get full text
    Get full text
    Proceeding Paper
  17. 57

    Experimental investigation of the vortical flow around a reverse delta wing using PIV by Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar

    Published 2010
    “…Particle Image Velocimetry was used in a low speed wind tunnel to investigate the vortex structures of a slender reverse delta wing at various angles of attack and roll. This work investigates the characteristics of the vortices generated downstream in a plane perpendicular to the free stream direction and their dependence on angles of attack and roll angles at chord based Reynolds number.…”
    Get full text
    Proceeding Paper
  18. 58

    Prediction of energy absorption capability of curved panel structure; for wing leading edge study by Omar, Norihan, Md Khalid, Nur Aisyah, Shamsudin, Nor Fadilah, Aminanda, Yulfian

    Published 2012
    “…This paper works on the curvature effect of wing leading edge structure subjected to impact loading. …”
    Get full text
    Article
  19. 59

    Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure by Omar, Nurihan, Aminanda, Yulfian, Syed Mohamed Ali, Jaffar

    Published 2014
    “…This paper works on the curvature composite structure for wing leading edge application using fabric carbon/epoxy material subjected to impact loading. …”
    Get full text
    Get full text
    Article
  20. 60

    Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow by Crasta, Asha, Khan, Sher Afghan

    Published 2016
    “…In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. …”
    Get full text
    Article