Transforming the Shock Pattern of Supersonic Jets Using Fluidic Injection-Reference-Cited by-同舟云学术

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Transforming the Shock Pattern of Supersonic Jets Using Fluidic Injection

Published:2019-05 Issue:5 Volume:57 Page:1851-1861
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Semlitsch Bernhard¹,Cuppoletti Daniel R.²,Gutmark Ephraim J.³,Mihăescu Mihai⁴

Affiliation:

1. University of Cambridge, Cambridge, England CB3 0DY, United Kingdom

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

3. University of Cincinnati, Cincinnati, Ohio 45221-0070

4. Royal Institute of Technology, 10044 Stockholm, Sweden

Funder

Swedish National Infrastructure for Computing

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057629

Reference29 articles.

1. Parametric Testing of Chevrons on Single Flow Hot Jets

2. An MDOE Investigation of Chevrons for Supersonic Jet Noise Reduction

3. Understanding How Chevrons Modify Noise in Supersonic Jet with Flight Effects

4. BridgesJ.WernetM.BrownC. “Control of Jet Noise Through Mixing Enhancement,” NASA TM 212335, 2003.

5. The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet

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1. Rectangular Sonic Jet Control with Supersonic Fluidic Injectors;Journal of Aerospace Engineering;2024-05

2. Air tab location effect on supersonic jet mixing;International Journal of Turbo & Jet-Engines;2024-04-04

3. Internal Fluidic Injection for the Control of Supersonic Rectangular Jet Noise;AIAA SCITECH 2024 Forum;2024-01-04

4. Forced Injection of a Spanwise-Inclined Jet in Supersonic Crossflow;AIAA Journal;2024-01

5. Performance Analysis of Fluidic Injector for Supersonic Jet Manipulation;AIAA Journal;2023-11-02

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