Mohammed Khalil Ibrahim
Professor and Head of Aerodynamics Group
Faculty of Engineering, Aerospace Engineering Department, Cairo University, Giza 12613, Egypt (email)
Aerodynamics Laboratory @ Nagoya University
Contrbutions to Aerodynamics Laboratory @ Aerospace Engineering Department, Nagoya University
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Development of Transmission Loss Measurement System, JAXA Funded Project, (2008-2009)
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Development of Pressure Senstive Paint System for Turbomachine Applications, Nogoya University Center of Excellence (COE) Funded Project, (2006-2009)
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Development of Automatic Measurement System for For High Speed Jet Acoustic Measurement, 2008
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Development of Automatic Measurement System for For Turlulance Measurements in Duct Flows, Funded Project By Denso-Techno in Japan, 2009
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Design, Build, and Testing of Anechoic Room, JAXA Funded Project, 2009
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Development of Miniature Quadraotor, EQUOS RESEARCH CO., LTD Funded Project, (2005 - 2013)
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Construction of Supersonic Windtunnel Exit Silencer (2009)
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Suppression of The Supersonic Windtunnel Diffuser Noise (2008)
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Development of Low Speed Wake Survey System (2007)
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Attitude Control of Rover (2010)
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Establishing of Rapid Modeling Workshop (2006)
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Low Turbulence and Low Speed Wind Tunnel Trouble-shooting (2006)
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Conducting Experiments at Japan's Largest Supersonic Windtunnel, July 2008
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Upgrading the Low Speed Windtunnel Power Unit, November 2011
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Conducting Students Experiments at Nagoya University, Aerodynamics Labratory, Japan 1998.
