A Gas Turbine Compressor Simulation Model for Inclusion of Active Control Strategies

Abstract

A one dimensional time-marching model to solve the dynamic behavior of a compression system is presented. The computational method is described in some details and it is applied to a three-stage axial compressor with different plenum configurations. This computational model for the simulation of a multistage axial compressor is used to investigate the insertion of an active control system.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2001
Accession Number
ADP011157

Entities

People

  • Aristide Massardo
  • Carlo Cravero

Organizations

  • University of Genoa

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Axial Flow Compressors
  • Centrifugal Compressors
  • Compression
  • Compressors
  • Computational Fluid Dynamics
  • Computational Science
  • Control Systems
  • Flow Rate
  • Fluid Dynamics
  • Fluid Mechanics
  • Gas Turbines
  • Military Aircraft
  • Static Pressure
  • Steady Flow
  • Three Dimensional
  • Vehicles

Fields of Study

  • Engineering
  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Robotics and Automation.