International Conference Contrbutions

  1. Mohammed K. Ibrahim, ""On the Noise Emission due to the Interaction of a High Speed Jet with a Soild Boundary", First Aviation Engineering Innovation Conference AEIC-1, March 21-22, 2015, Luxor, Egypt.[PDF]
  2. Rei Kawashima, Cho Mengu, and Mohammed K. Ibrahim, “Challenges and Opportunities of UNISEC-Global”, International Astronautical Congress, October, Toronto, 2014. [PDF]
  3. Mohammed K. Ibrahim, Mohamed Yunus, and Ahmed Z. Al-Garni, “Numerical Investigation of High Speed Jets – Generated Edge-tones” 10th European Fluid Mecahnics Conference (EFMC10), Copenhagen, September 14-18, 2014.[PDF]
  4. Mohammed K. Ibrahim and Ahmed Z. Al-Garni, “Attitude Dynamics of Nano-Satellite due to Full Orbit Perturbations”, 5th International Nano-satellite symposium November 20-22, 2013, Tokyo, Japan.[PDF]
  5. Hassan Aly, Omar Sharkawy, Ashraf Nabil, Ahmed Yassin, Mohamed Tarek, Samy M. Amin, and Mohammed K. IBRAHIM, “Project-based Space Engineering Education: Application to Autonomous Rover-Back CanSat”, 6th  International Conference on Recent Advances in Space Technologies (RAST), June 12-14, 2013,  Istanbul, Turkey.[PDF]
  6. Mohammed K. IBRAHIM, Nobuhiro Miya, Takaaki Yumitori, and Yoshiaki Nakamura, “Noise Suppression of Underexpanded Sonic Jet by Finite Tube Attachment”, 29th International Symposium on Space Technology and Science (ISTS), June 2-9, 2013, Nagoya, Japan [PDF]
  7. Celebi, M. Mohammed K. IBRAHIM, Aydemir, M.E., Bensaada M., Fernando L. H. J. D. K., Akiyama, H., Yamaura, S. “Design and Navigation Control of an Advanced Level CANSAT”, 5th International Conference on Recent Advances in Space Technologies (RAST), June 9-11, 2011, pp/ 856-860, Istanbul, Turkey. [PDF]
  8. Mahmoud M. El-GENDI, and Mohammed K. IBRAHIM,  "Effect of Turbulence Model on the Calculated Flow through Rectilinear Turbine Cascade" The Second International Conference of Energy Engineering; ICEE-2, 27-29 December 2010, Aswan, Egypt.[PDF]
  9. Mohammed K. IBRAHIM, Koichi Mori , and Yoshiaki Nakamura, “Visualization of Flow Field over Rotating Blades using Pressure Sensitive Foil Technique”, 47th  AIAA Aerospace Sciences Meeting and Exhibit, World Center Marriott Orlando, Florida, 5-8 January 2009, AIAA 2009-1076. USA. [PDF]
  10. Mahmoud El-Gendi, Mohammed K. IBRAHIM, Koichi Mori, and Yoshiaki Nakamura, “Elliptic Trailing Edge for a High Subsonic Turbine Cascade”, KSAS-JSASS Joint International Symposium on Aerospace Engineering, 20-21 November, 2008, Ramada Plaza Jeju Hotel , Jeju, Korea.[PDF]
  11. M. El-Gendi, Mohammed K. Ibrahim, Mori, and Y. Nakamura "Effect of Trailing Edge Geometry on a Turbine Blade Base Pressure" In Proceedings of International Symposium on Frontiers of Computational Science, pages 197-204, 2008. [PDF]
  12. Mohamed El-Ghandour, Mohammed K. IBRAHIM, Koichi Mori, and Yoshiaki Nakamura, “A Triple Squealer For Axial Flow Turbines”, KSAS-JSASS Joint International Symposium on Aerospace Engineering, 20-21 November, 2008, Ramada Plaza Jeju Hotel , Jeju, Korea. [PDF]
  13. Igor Menshov, Ilya Semenov, Ildar Ahmedyanov, Mohammed k. IBRAHIM, and Yoshiaki Nakamura, “Towards Understanding the Physics of Supersonic Jet Screech”, The Fifth International Conference of Computational Fluid Dynamics – ICCFD5, Seoul, KOREA July 7-11, 2008. [PDF]
  14. Mohammed K. IBRAHIM, Koichi Mori , and Yoshiaki Nakamura, “Application of Pressure Sensitive Foil Technique to Visualize Subsonic Jet Flow over a Plate”, 13th International Conference on Applied Mechanics and Mechanical Engineering, AMME-13, May 27-29, 2008, Cairo, Egypt. [PDF]
  15. Hiroshi Ozawa, Katsuhisa Hanai, Mohammed K. Ibrahim, Koichi Mori and Yoshiaki Nakamura, “Experimental Analysis of TSTO Aerodynamic Heating Problems at Hypersonic Speed”, AIAA Paper 2008-2671, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, April 28 - May 1, 2008, Dayton Convention Center, Dayton, Ohio, USA. [PDF]
  16. Ochi, A. Mohammed K. Ibrahim, and Nakamura, Y. “CFD Validation Study of Wake Capturing Capability for Flat Plate Wake”, 37th  AIAA Fluid Dynamics Conference & Exhibit, 25-28 June 2007, Anaheim, CA, AIAA Paper 2007-4195, USA. [PDF]
  17. Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, and Yoshiaki Nakamura, “Numerical Simulation of Trailing Edge Vortex Shedding in a High Subsonic Turbine Cascade”, JSASS-KSAS Joint International Symposium on Aerospace Engineering, October 10-12, 2007, Kitakyushu, Japan. [PDF]
  18. Mohammed K. IBRAHIM, “Visualization of Underexapnded Jet Flows over a Plate by Pressure-Sensitive Paint Technique”, 12th International Conference on Aerospace Sciences and Aviation Technology, May 29-31, 2007 Cairo, Egypt. [PDF]
  19. Mohammed K. IBRAHIM,  Souma, T., and Nakamura, Y. "Suppression of Edge-Tones in High-Speed Flows," JSASS 5th International Sessions in 39th Aircraft Symposium October 29-31, 2001, Nagaragawa Convention Center, Gifu, Japan. [PDF]
  20. Mohammed K. IBRAHIM, Kunimura, R.  and Nakamura, Y. "Spreading Enhancement of Axisymmetric Supersonic Jet by the Use of Micro Jets," 31st AIAA Fluid Dynamics Conference & Exhibit, 11-14 June 2001, Anaheim, CA, AIAA Paper 2001-3048, USA. [PDF]
  21. Mohammed K. IBRAHIM, and Nakamura, Y. "Suppression of Supersonic Jet Noise by Free-to-Rotate Vane-Type Tabs," JSASS 13th International Session in 37th Aircraft Symposium, Ota-Ku Sangyo Plaza, 13-15 October 1999 ,Tokyo, Japan.[PDF]
  22. Mohammed K. IBRAHIM, and Nakamura, Y. "Flow Field and Noise Characteristics due to Supersonic Jet Shear Layer-Vortex Interaction," AIAA Fluids 2000 Conference and Exhibit, 19-22 June 2000, Denver, Colorado, AIAA Paper 2000-2533, USA. [PDF]
  23. Mohammed K. IBRAHIM, and Nakamura, Y. "The Effects of Vane-Type Tabs on Flow and Acoustic Fields of Supersonic Jet," 38th Aerospace Sciences Meeting & Exhibit, 10-13 Jan 2000, Reno, NV, AIAA Paper 2000-0087, USA. [PDF]
  24. Sherif, A. O. and Mohammed K. IBRAHIM, "Grid Type Effects on Two-Dimensional Euler Computation," Proceeding of Al-Azhar Engineering Fifth International Conference, Cairo AEIC'97, Dec. 19-22, 1997, Egypt. [PDF]
  25. Mohammed K. IBRAHIM, and Sherif, A. O. "A Two-Dimensional Flux Vector Splitting Euler Solver," Proceeding of fifth International Conference of Fluid Mechanics, Cairo, ICFM5 Vol. II (1995), pp. 621-635, Egypt.[PDF]