Accession Number:

ADA361702

Title:

Design Principles and Methods for Aircraft Gas Turbine Engines Les Principes et Methodes de Conception des Turbomoteurs

Descriptive Note:

Proceedings

Corporate Author:

NATO RESEARCH AND TECHNOLOGY ORGANIZATION NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1999-02-01

Pagination or Media Count:

491.0

Abstract:

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.

Subject Categories:

  • Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE