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Posted By: | Nitin Jain |
Date: | Mon, 17 May 2010, 3:27 p.m. |
Thursday, June 3, 2010, 10:00 AM – 11:00 AM EST
Register: http://www.conceptsnrec.com/events_webinar.html
Demonstration Case: An Axial Turbine for an Aircraft Propulsion Application
Challenge: Reduce the turbine stage count, while still maintaining the power and efficiency level.
Solution: Accelerated redesign of the turbine using Concepts NREC's Agile Engineering Design System® to reduce weight and machining costs and still meet the performance requirements.
In this Webinar, Mark Anderson, Vice President of Software Development at Concepts NREC, will go through a step-by-step process of redesigning a low pressure axial turbine from 3 stages down to 2. The live demonstration will highlight all the major components of design process including: preliminary design (meanline), advanced geometry layout, quasi-3D CFD (Computational Fluid Dynamics) analysis, and full 3D CFD.
Register: http://www.conceptsnrec.com/events_webinar.html
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