Core Engine Noise Control Program. Volume III. Prediction Methods

Abstract

Prediction methods for core engine noise were reviewed and either updated or new noise evaluation techniques formulated for low velocity coannular jets, combustors ('core' noise), Low pressure turbines, interaction between turbine tones and fan/core jet streams, obstructions in the flow passages and casing radiation. The development was based, to a large extent, on the analytical investigation and the model, component and engine tests evaluated during Phases 2 and 3 of this program. The results were cast in a general form, so as to be applicable to a wide variety of cycles, including present and future turbofan engines. The prediction methods were validated with measured acoustic data wherever possible.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1974
Accession Number
ADA013131

Entities

People

  • D. Latham
  • J. J. Emmerling
  • K. R. Bilwakesh
  • R. K. Matta
  • S. B. Kazin

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Acoustics
  • Bandwidth
  • Boundary Layer
  • Carburetors
  • Combustion
  • Engine Noise
  • Frequency Bands
  • Gas Turbines
  • High Bypass Turbofans
  • Rotor Blades (Turbomachinery)
  • Test Facilities
  • Turbine Components
  • Turbines
  • Turbofan Engines
  • Turbojet Engines
  • Turboshaft Engines
  • Turbulent Mixing

Readers

  • Acoustics.
  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation