Rotating Stall in an Axial Flow Single Stage Compressor. On-Blade Velocity Measurements.

Abstract

Three multiple hot wire sensors are developed and applied to a low speed axial compressor rotor blade. The multiple wire sensor design is based on the technique of the combined hot and cold wire in a parallel arrangement for the detection of flow separation and reversal. The sensors are used in the unstalled and stalled part of the compressor characteristics with one and two stall cells present. The signals are analyzed using the fast Fourier transform, power spectra and correlation techniques. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 15, 1982
Accession Number
ADA114627

Entities

People

  • B. Gyles
  • F. A. E. Breugelmans
  • P. Ligrani

Organizations

  • von Kármán Institute for Fluid Dynamics

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Axial Flow
  • Axial Flow Compressors
  • Boundary Layer
  • Compressor Blades
  • Compressor Rotors
  • Computational Fluid Dynamics
  • Detectors
  • Equations Of Motion
  • Flow Fields
  • Fluid Dynamics
  • Geometry
  • Guide Vanes
  • Inlet Guide Vanes
  • Measurement
  • Power Spectra
  • Pressure Measurement
  • Spectra

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Sensor Fusion and Tracking Systems.