Basic Studies of Rotating Stall in Axial Flow Compressors.

Abstract

This report presents the results of a theoretical and experimental program aimed at obtaining a sufficient understanding of the rotating stall phenomena such that its onset and properties can be predicted under a wide set of circumstances. The theoretical research covers the development of two-dimensional stability theories for compressible flows and the progress towards the development of a three-dimensional theory for incompressible flow. The experimental work, performed in an annular cascade facility, studied the effects of rotorstator interference both on the steady-state performance of the blade rows and on rotating stall. The influence of circumferential distortion on the rotating stall boundary for the stage was also determined. Comparisons are made between the experimental results and the predictions of a two-dimensional rotating stall stability theory which had been developed previously for incompressible flows. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1979
Accession Number
ADA077690

Entities

People

  • Gary R. Ludwig
  • Joseph P. Nenni

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axial Flow Compressors
  • Back Pressure
  • Boundary Layer
  • Compressible Flow
  • Computational Fluid Dynamics
  • Distortion
  • Dynamic Pressure
  • Fluid Dynamics
  • Hydrodynamics
  • Incompressible Flow
  • Measurement
  • Pressure Measurement
  • Rotors
  • Static Pressure
  • Steady Flow
  • Steady State
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Theoretical Analysis.