Aerodynamics Laboratory @ Nagoya University

Contrbutions to Aerodynamics Laboratory @ Aerospace Engineering Department, Nagoya University

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

Mohammed Khalil Ibrahim