Design Principles and Methods for Aircraft Gas Turbine Engines Les Principes et Methodes de Conception des Turbomoteurs
NATO RESEARCH AND TECHNOLOGY ORGANIZATION NEUILLY-SUR-SEINE (FRANCE)
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The 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 CombustorsAugmentors 4 papers Compressor Systems Part I 5 papers Compressor Systems Part II 3 papers Turbines Part I 5 papers Turbines Part II 4 papers Engine Design and Analysis Part II 4 papers These proceedings also include a Technical Evaluation Report and a Keynote address published in French and English.
- Jet and Gas Turbine Engines