Mohammed Khalil Ibrahim
Professor and Head of Aerodynamics Group
Faculty of Engineering, Aerospace Engineering Department, Cairo University, Giza 12613, Egypt (email)
BSc Thesis Advised
- Orbit Determination and Analysis of Cubesat for Information Collecting Mission, King Fahd University of Petroleum and Minerals, May 2013.
- Design, Fabrication and Fly of an Autonomous Quad-rotor VTOL Vehicle, Cairo University, July 2012. (Won the best Mechanical Engineering Project in the Egyptian Engineering Day 2012)
- Design, Fabrication and Test of Rover-Back CanSat for Space Engineering Education, Cairo University, July 2012.
- Design, Fabrication and Fly of an Autonomous Blimp for Terrain Mapping, Cairo University, July 2011.
- Design, Fabrication and Test of Soda-Can Size Satellite for Space Engineering Educations, 2011. (Won the best Mechanical Engineering Project in the Egyptian Engineering Day 2011)
- Design of Liquid Oxidizer Hybrid Rocket Engine, Cairo University, July 2010.
- Experiments of Flow Separation Suppression on the Flap Upper Surface with the Moving-Surface, Nagoya University, Feb. 2009.
- Modeling and Analysis of Hot-Dip Galvanizing Line, Nagoya University, Feb. 2009.
- Experiments on Sound Transmission Characteristics with Acoustically Induced Vibration of CFRP Thin plates, Nagoya University, Feb. 2009.
- Development of Test Rig for the Application of Pressure Sensitive Paint for Turbo-Machine Application, Nagoya University, Feb. 2008.
- Design, Fabrication and Realization Quad Rotor Flying Robot, Nagoya University, Feb. 2008.
- Design, Fabrication and Realization of an Acoustic Test Facility for Noise and Vibration Study of Space Launching System, Nagoya University, Feb. 2008.
- Experimental Investigation of Flow Field around a Canopy at Subsonic Speeds, Nagoya University, Feb. 2007.
- Experimental and Theoretical Study of Flow Induced Noise over Circular Cylinder at Subsonic Speeds, Cairo University, July 2006.
- Development of The Pressure Sensitive Paints Technique for High and Low Speed Aerodynamic Applications, Cairo University, July 2006.
- Experimental Investigation of Aerodynamics Characteristics of flow around Delta wing of Aspect Ratio 1.3 at Low Subsonic Speed, Cairo University, July 2005.
- Design, Fabrication Testing of a Supersonic Wind Tunnel for Educational Purposes, Cairo University, July 2005.
- Design of Short Range Civil Airplane, Institute of Aviation Engineering and Technology, Egypt, July 2004.
- Flow Measurements and Visualization in Subsonic Wind Tunnels, Cairo University, July 2004.