Numerical Investigation of Supersonic Jet Noise Suppression via Downstream Microjet Fluidic Injection-Reference-Cited by-同舟云学术

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Numerical Investigation of Supersonic Jet Noise Suppression via Downstream Microjet Fluidic Injection

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Pourhashem Hamideh¹,Kalkhoran Iraj M.¹

Affiliation:

1. NYU Tandon School of Engineering

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0002

Reference40 articles.

1. On the energy scattered from the interaction of turbulence with sound or shock waves

2. Ribner, H.S, "Convection of a pattern of vorticity through a shock wave, " NACA Report 1164, 1954(supersedesNACA TN-2864, 1953).

3. Directional Suppression of Noise from a High-Speed Jet

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2. RANS Simulations of Thermally Non-Uniform Supersonic Jets;AIAA AVIATION 2020 FORUM;2020-06-08

3. Flow field characteristics of a supersonic jet influenced by downstream microjet fluidic injection;Aerospace Science and Technology;2019-10

4. Bow Shock/Vortex Interaction: Effect of Reducing the Vortex Height on Structure of the Generated Flow Field;AIAA Scitech 2019 Forum;2019-01-06

5. LES of Unheated and Heated Supersonic Jets with Fluidic Injection;2018 AIAA Aerospace Sciences Meeting;2018-01-07

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