Two-point radiation statistics from large-scale turbulent structures within supersonic jets

Abstract

The noise from large-scale coherent turbulent structures within jets remains the dominant source. For the purpose of developing future control systems for the large-scale noise source, we investigate the statistics between upstream and downstream radiating waves. We investigate two off-design supersonic jet flows with instability theory and associated noise radiation, large-eddy simulation (LES), and experiments. We compare the auto-correlation, cross-correlation, coherence, and other statistics predicted by aeroacoustic instability theory. As instability waves are closely connected with the formation of large-scale turbulent structures, they yield insight into large-scale noise statistics. We investigate two nozzles at two supersonic off-design conditions. The first is a biconic nozzle operating at an unheated condition, and the second is a NASA nozzle operating at a heated condition. We find that for these jets, the noise from instability waves is coherent between 0.40 to 0.70 at large-scale radiation frequencies between the downstream and upstream radiation directions.

Document Details

Document Type
Pub Defense Publication
Publication Date
Apr 13, 2021
Source ID
10.1177/1475472x211005413

Entities

People

  • James D Goldschmidt
  • Jianhui Cheng
  • Lawrence S Ukeiley
  • Steven Miller
  • Weiqi Shen

Organizations

  • Strategic Environmental Research and Development Program
  • University of Florida

Tags

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow