Modern Prediction Methods for Turbomachine Performance

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.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1976
Accession Number
ADA028337

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Gas Turbines
  • Heat Transfer
  • Hybrid Power
  • Hydrodynamics
  • Mathematical Filters
  • Rotor Blades (Turbomachinery)
  • Test Facilities
  • Turbine Components
  • Turbogenerators
  • Turbulent Mixing

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Systems Analysis and Design