Unsteady Effects of Circumferential Pressure Distorted Inlet Flows in Compressors.

Abstract

A high response measuring and data acquisition system is described which has been custom designed and built for the research facility used in this investigation. The system included the potential for measuring instantaneous dynamic pressures on rotor blades in unsteady flow and the real-time analysis of data or alternatively data storage for off-line analysis. (Author)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1978
Accession Number
ADA062549

Entities

People

  • R. E. Peacock

Organizations

  • Cranfield University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Analogs
  • Centrifugal Force
  • Compressors
  • Data Analysis
  • Dynamic Response
  • Engineering
  • Flow
  • Fluid Flow
  • Frequency
  • Frequency Response
  • Instrumentation
  • Mechanical Engineering
  • Microprocessors
  • Pressure Measurement
  • Pressure Transducers
  • Resonant Frequency
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Test and Evaluation
  • Robotics and Automation.