DYNAMICS OF ACOUSTICALLY COUPLED COMBUSTION INSTABILITIES RELEVANT TO ROCKET PROPULSION SYSTEMS

Abstract

Over the past several years, experiments at UCLA have explored several alternative fuel injectors, for a range of flow conditions and for different acoustic excitation conditions, many of which are similar to or exceed the relative amplitude of acoustic excitation performed at AFRL.

Document Details

Document Type
DoD Grant Award
Publication Date
Mar 07, 2023
Source ID
FA95502210190

Entities

People

  • Ann Karagozian

Organizations

  • Air Force Office of Scientific Research
  • United States Air Force
  • University of California, Los Angeles

Tags

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Internal Combustion Engine (ICE) Technology.
  • Technical Research and Report Writing.