Propagating Potential Disturbances in Turbomachinery

Abstract

This report documents the work performed at Notre Dame on attempting to acquire a clean set of phase-locked unsteady velocity data and concomitant unsteady pressure response for upstream-propagating potential disturbances interacting with a sharp-trailing-edged cascade vane in compressible, subsonic flow. The report documents the importance of the work and classifies the types of potential-disturbance interactions that can occur in a turbine engine. A case is made for the importance of the Notre Dame cascade approach, which allows for unambiguous interpretation of the data if the potential-disturbance sources are properly phased. The relationship of the Notre Dame cascade efforts to related work being conducted using a running F109 turbofan engine is described. The specially-designed cascade section is described along with a description of some of the preliminary results. Based on analysis of these results, a case is made for concentrating on a control method for phasing the potential-disturbance generators.

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Document Details

Document Type
Technical Report
Publication Date
Mar 02, 2002
Accession Number
ADA400117

Entities

People

  • Eric J. Jumper

Organizations

  • University of Notre Dame

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Materials and Manufacturing Processes
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Engines
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Gas Turbines
  • Hydrodynamics
  • Leading Edge Flaps
  • Mechanical Engineering
  • Physics Laboratories
  • Turbines
  • Turbofan Engines
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Theoretical Analysis.