Conference Proceedings

SCOPUS Conference

  1. Mat, S., Abdullah, M. F., Dahalan, M. N., Said, M., Mansor, S., Abdul Latif, A., and Mat Lazim, T. (2017). Effects of Synthetic Jet Actuator (SJA) on Flow Topology of Blunt-Edged UTM VFE2 Wing Model. 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum. 9 – 13 January. Grapevine, Texas.
  2. Said, M., and Mat, S.(2016). Effects of Reynolds Number On the Onset of Leading Edge Vortex Separation Above Blunt-Edge Delta Wing VFE-2 Configurations. 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016. 25 – 30 September. Daejeon, Korea.
  3. Kasim, K. A., Mat, S., Ishak, I. S., and Said, M. (2016). Effects of propeller locations on the vortex system above delta-shaped UAV model. 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016. 25 – 30 September. Daejeon, Korea. ISBN: 9783932182853.
  4. Said, M., Mat, S., Mansor, S., Abdul-latif, A., and Mat Lazim, T. (2015). Reynolds Number Effects on Flow Topology Above Blunt-Edge Delta Wing VFE-2 Configurations.53rd AIAA Aerospace Sciences Meeting. 5 – 9 January. Kissimmee, United States.
  5. Coton, F. N., Mat, S., Galbraith, R., and Gilmour, R. (2009). The Effect of Leading Edge Radius on a 65 of Delta Wing.47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. 5 – 8 January. Orlando, Florida.
  6. Coton, F., Mat, S., Galbraith, R. and Gilmour, R. (2008). Low Speed Wind Tunnel Characterization of the VFE-2 Wing.  46th AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings. 7 – 10 January, Rano, Nevada, pp. 1-10.
  7. Azahar, N.I.N, Mat Lazim, T., and Mat, S. (2019). Verification Verification of heat transfer enhancement in tube with spiral corrugation. The 10th International Meeting of Advances in Thermofluids (IMAT 2018). Vol 2062. pp. 020032-1–020032-8.
  8. Ujang, M. I., Mat, S., Perumal, K., and Mohd Nasir, M. N. (2016). Experimental study of UTM-LST generic half model transport aircraft. AEROTECH VI – Innovation in Aerospace Engineering and Technology. Vol 152. pp. 1-8.
  9. Amir, M. A. U., Maimun, A., Mat, S., Saad, M. R. (2016). Computational analysis of aerodynamic characteristics for wing in ground effect craft in lateral stability. AEROTECH VI – Innovation in Aerospace Engineering and Technology. 152(1), 1-9.
  10. Mat, S., Ishak, I.S, Zakaria, K. & Khand, Z.A. (2014). Manufacturing process of blended delta-shaped wing model. dvanced Materials Research Volume 845, 2014, Pages 971-974