An Attempt to Correlate Normal Vorticities with Total Pressure Distortion Patterns at the Entrance to a Gas Turbine Engine

Abstract

An attempt is made to predict the worst-case pressure distortion produced by a distortion screen at the entrance to a gas turbine engine using only steady-state total pressure measurements. The vector sum of radial and circumferential vorticity, called normal vorticity, is compared to both the difference between steady-state and worst-case distortion patterns, and the standard deviation of the high response pressure measurements, called turbulence. Average values of turbulence and vorticity are found to be unrelated to the increase in distortion between steady-state and worst-case pressure measurements. Probe-by-probe analysis of the data indicates that a correlation may exist between vorticity and the distortion increase. Although a final prediction technique is not developed, an improved test program and refined data analysis techniques are outlined.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1977
Accession Number
ADA040370

Entities

People

  • Stephen M. Clark

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Compressors
  • Computer Programs
  • Data Analysis
  • Equations
  • Fluid Flow
  • Gas Turbines
  • Instrumentation
  • Mach Number
  • Plastic Explosives
  • Pressure Gradients
  • Pressure Measurement
  • Simulators
  • Static Pressure
  • Steady State
  • Test Facilities
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Applied Combinatorial Optimization and Logic Circuit Design.
  • Fluid Mechanics and Fluid Dynamics.