BASIC STUDIES OF ROTATING STALL AND AN INVESTIGATION OF FLOW-INSTABILITY SENSING DEVICES. PART I. BASIC STUDIES OF ROTATING STALL FLOW MECHANISMS.

Abstract

The report describes an experimental and analytical investigation of flow processes basic to the problem of rotating stall in axial flow compressors. Boundary-layer studies show that simple analytical treatment of flow separation on a wall moving upstream is not feasible, whereas, partial analytical success was obtained for flow separation on a wall moving down-stream. A stability theory for small disturbances propagating rotationally in the mean swirled flow through a thin annulus with multiple actuators (blade rows) was derived. Comparisons with experimental rotating stall data show fair-to-good agreement of propagation velocities but inaccurate predictions of inception of instability. Additional research is proposed related to lift hysteresis on airfoils in separated flows, time-delay inherent in the leading-edge separation process, and modification and extension of the developed stability theory. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625783

Entities

People

  • G. R. Ludwig
  • W. G. Brady

Organizations

  • Calspan

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Actuators
  • Agreements
  • Axial Flow
  • Axial Flow Compressors
  • Boundaries
  • Boundary Layer
  • Compressors
  • Flow
  • Flow Separation
  • Hysteresis
  • Instability
  • Layers
  • Leading Edges

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.