... ,” Proceedings of the IEEE Aerospace Conference . 04 06 2010 28 06 2010 06 05 2011 06 05 2011 aerospace computing aircraft data mining The CF-18 has been in service with the Canadian Forces (CF) since the early 1980s. The first aircraft was delivered in October 1982...

... due to the transient fuel flow change using the Runge–Kutta method. In this transient performance simulation, the turbine overshoot was predicted. 31 03 2008 09 04 2008 10 02 2009 aerospace computing aerospace engines aerospace propulsion aircraft control control engineering...

... 3.6238 Bearing chamber C 3.8 3.6993 14 04 2008 15 05 2008 10 02 2009 aerospace computing aerospace engines flow simulation gears heat exchangers lubricating oils lubrication machine bearings nozzles numerical analysis orifices (mechanical) pipes temperature...

... is very important for the overall gain in efficiency of the complete engine. heat exchangers aerospace engines matrix algebra heat transfer stress analysis thermal analysis finite element analysis creep dynamic testing cooling aerospace computing 01 October 2003 01 March...

... (SFC) is increasing as in Figs. 9e 9f . Therefore, this case thrust oscillation should also be considered for safe flight during flight mode transition. 25 08 2005 28 09 2005 jet engines aerospace propulsion rotors aerospace computing mathematics computing valves...

.... aerospace engines Kalman filters quadratic programming aerospace computing state estimation parameter estimation 16 June 2003 01 October 2002 01 March 2003 15 04 2005 Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL...

... aerospace computing CAD aerospace engines software packages graphical user interfaces aerospace propulsion systems analysis During the preliminary design phase of gas turbines the main parameters are fixed. These, in return, fix most of the risks and financial resources associated...

... aerospace materials mass aerospace computing Engine weight is a key design parameter for any new aircraft engine. It affects aircraft range and is a key element in fuel burn. Weight is also considered an indicator of engine cost. Reliable engine-weight estimation at the conceptual design stage...

...-friendly graphical user interface (GUI) is available to handle the otherwise difficult task of setting up the problem for analysis and viewing the results. aerospace engines gas turbines rotors probability aerospace computing fatigue testing 03 June 2002 01 Dec 2001 01 Mar...

... ‐ deg intervals. Grid layout for three-stage fan 01 10 2003 01 03 2004 numerical analysis aerospace engines aerospace propulsion aerospace computing fans distortion The research reported herein was performed by the Arnold Engineering Development Center...

... by IGTI, December 2001, final revision, March 2002. Associate Editor: E. Benvenuti. 03 June 2002 01 December 2001 01 March 2002 15 08 2003 gas turbines electric sensing devices neural nets fault diagnosis aerospace engines aerospace instrumentation aerospace computing...