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Design Principles and Methods for Aircraft Gas Turbine EnginesThe symposium dealt with design approaches for military aircraft propulsion systems to provide enhanced operational flexibility, longer range, better fuel efficiency and improved affordability. All classes of gas turbines were addressed in nine sessions as follows: Engine Design and Analysis (Part 1) (5 papers); Mechanical Systems (6 papers) Controls (4 papers); Combustors/Augmentors (4 papers); Compressor Systems (Part 1) (5 papers); Compressor Systems (Part 2) (3 papers); Turbines (Part 1) (5 papers); Turbines (Part 2) (4 papers); and Engine Design and Analysis (Part 2) (4 papers). These proceedings also include a Technical Evaluation Report and a Keynote address published in French and English.
Document ID
Document Type
Conference Proceedings
Date Acquired
August 19, 2013
Publication Date
February 1, 1999
Publication Information
Publication: Design Principles and Methods for Aircraft Gas Turbine Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-837-0005-8
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Meeting Information
Meeting: RTO Applied Vehicle Technology Panel (AVT) Symposium
Location: Toulouse
Country: FR
Start Date: May 11, 1998
End Date: May 15, 1998
Sponsors: North Atlantic Treaty Organization
Distribution Limits
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