Noise of High-Performance Aircraft at Afterburner

Abstract

Numerical simulation of the generation of indirect combustion noise in a military styled nozzle at afterburner.

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Document Details

Document Type
Technical Report
Publication Date
Sep 22, 2016
Accession Number
AD1017458

Entities

People

  • Christopher Tam

Organizations

  • Florida State University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Acoustics
  • Aircrafts
  • Algorithms
  • Combustion
  • Computations
  • Cross Correlation
  • Engine Noise
  • Equations
  • Flow
  • Frequency
  • Mach Number
  • Military Aircraft
  • Noise
  • Pressure Distribution
  • Simulations
  • Three Dimensional
  • Turbofan Engines