Home
Technical Program
Author Center
Event Information
Help
Login
 

Session Schedule
Event Schedule
Review Process
Registration
Hotel Reservations
Short Courses
Exposition Opportunities
Information for Exhibitors
Exhibitor Directory
Sponsorship Opportunities
Facility Tours
Guest Tours
Press Room
Organizers

Contact Us

Acceptance notification, technical content, etc.
Volunteer Organizers

Program, events, etc.
Stephanie Sears

Expositions, sponsorships, etc.
Kristin Barranger

Copyright forms
copyright@asme.org

Website support
igtiprogram@asme.org

 
Short Course

"Gas Turbine Aerothermodynamics and Performance Modeling"

A two-day short course in conjunction with Turbo Expo 2008

Saturday, June 7 & Sunday, June 8, 2008 - Berlin, Germany


Short Course Fee: €950
SAVE!!! Reduce your fee to €750 by Registering for 2008 Turbo Expo Technical Congress and Providing Your Registration Confirmation Number!
Short Course fee includes lunch, refreshment breaks and course materials.


Instructor
Syed Khalid, Chief Performance and Systems Integration Engineer on the JSF LiftFan at Rolls-Royce North America


This interactive course includes tutorial sessions in which the attendees can work out instructor-facilitated examples of gas turbine aerothermodynamics and performance modeling. The material has been evaluated by the Department of Mechanical and Aerospace Engineering at North Carolina State University. The course content will be useful to individuals involved with all types of gas turbine engines. The aircraft engine is used in the cycle analysis examples since several sophisticated techniques are utilized in such examples. However, the engineer can easily relate those examples to cycle analysis of other gas turbine engines. The presented aerothermodynamics and turbo-machinery theory is applicable to all types of gas turbine engines.


The highlights of the course are:

  • comprehensible presentation of the basic theory – freshman mathematics used
  • theory illustrated with worked out examples. Excel spreadsheets used
  • relevant thermodynamics and compressible fluid flow
  • physics of thrust generation and the function of turbo-machinery
  • generalized gas turbine performance parameters
  • energy transfer in a turbo-machine
  • basics of fan/compressor aerodynamic design
  • basics of turbine aerodynamic design
  • combustor performance characteristics
  • design point cycle analysis
  • integration of component performance to obtain mixed flow turbofan performance
    • design point calculations
    • off-design cycle balancing


Click here to register for this course. This 2-day course is a separate registration from the other pre-conference workshops and Turbo Expo.

 
 
  Sponsored By Media Sponsor
             
     
This site works best with: Internet Explorer 5.0+ Netscape 7.0+ Acrobat Reader 5.0+
Note to Firefox users: Firefox is not currently supported by the Conference Toolbox.

Copyright © 1996-2010 ASME. All Rights Reserved. Terms of Use | Privacy Statement
Powered by Conference Toolbox ™ version 4.0. For more information, contact us.