Aerothermodynamic Design Appraisal of Noise Suppressors for F/A-18 Engine Run-Up Facilities at RAAF Williamtown

Abstract

Upgraded facilities for ground running of F404 engines in F/A-18 aircraft at RAAF Williamtown will feature air-cooled exhaust augmentors for noise suppression. Aerothermodynamic aspects of the augmentor designs were appraised in some detail, making use of isothermal scale model tests, ejector theory and available empirical data. In initial design development, quantitative assessments were made of cooling flow pumping performance. Changes were recommended to improve the aerodynamic characteristics of the exhaust augmentors and eliminate high risk features, and the sizes of the augmentor ducts were significantly reduced. The model tests identified certain geometric features which were important for symmetry of the flow in the augmentor ducts and to pumping performance. Once modified accordingly, the designs displayed satisfactory aerodynamic behaviour, which was tolerant to both inlet asymmetries and reasonable levels of engine jet misalignment. The pumping performance was shown to exceed the design requirements.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1990
Accession Number
ADA236058

Entities

People

  • A. M. Abdel-fattah
  • S. A. Fisher

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Afterburners
  • Air Cooled
  • Aircrafts
  • Civil Aviation
  • Construction
  • Exhaust Gases
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Mechanics
  • Jet Engines
  • Mach Number
  • Measurement
  • Mechanical Engineering
  • Pressure Distribution
  • Static Pressure
  • Test Facilities

Readers

  • Aerospace Engineering
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Theoretical Analysis.