What is it about?

The present study shows a computational analysis of fluid injection as jet noise reduction technique for a supersonic jet. The research shows that the injectors reduce noise affecting the mechanism that generate broadband shock associated noise, and the large scale turbulent structures that generate the peak noise.

Featured Image

Read the Original

This page is a summary of: Large-Eddy Simulations Analysis of Supersonic Heated Jets with Fluid Injection for Noise Reduction, AIAA Journal, August 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057674.
You can read the full text:

Read

Contributors

The following have contributed to this page