Unsteady Effects of Circumferential Pressure Distorted Inlet Flows in Compressors.

Abstract

Using custom designed and developed rotor borne instrumentation rotating stall phenomena are examined in lightly loaded single-stage compressor. Two different classes of rotating stall are identified and of different rotational frequency. One propagates from the blade loading edge and the other from the blade trailing edge. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1978
Accession Number
ADA062550

Entities

People

  • R. E. Peacock

Organizations

  • Cranfield University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Compressors
  • Data Acquisition
  • Dynamic Pressure
  • Flow
  • Hydrodynamics
  • Instrumentation
  • Measurement
  • Mechanical Engineering
  • Observation
  • Pressure Distribution
  • Recording Systems
  • Stagnation Pressure
  • Static Pressure
  • Transducers
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.