Accession Number:

ADA028337

Title:

Modern Prediction Methods for Turbomachine Performance

Descriptive Note:

Lecture series

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1976-01-01

Pagination or Media Count:

168.0

Abstract:

Propulsion system development costs may be significantly reduced by improvement of methods for prediction of compressor and turbine component performance, and by preliminary study of the interactive operation of compressors and turbines with other system components. After the build-up of development engines, it is necessary to understand and carefully plan the process of rematching of components for optimum system performance.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE