Control of a Supersonic Rectangular Jet Using Plasma Actuators-Reference-Cited by-同舟云学术

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Control of a Supersonic Rectangular Jet Using Plasma Actuators

Published:2012-06-04 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Crawley Michael¹,Kearney-Fischer Martin¹,Samimy Mo¹

Affiliation:

1. Ohio State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2211

Reference50 articles.

1. Mach Wave Radiation from High-Speed Jets

2. Orderly structure in jet turbulence

3. Discrete Noise Spectrum Generated by Acoustically Excited Jet

4. Vortex pairing in a circular jet under controlled excitation. Part 1. General jet response

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Symmetric Mode-Mode Interactions in a Supersonic Rectangular Jet;AIAA SCITECH 2024 Forum;2024-01-04

2. Large-Eddy Simulations of Fundamental-Harmonic Coherent Structure Interactions in a Supersonic Rectangular Jet;AIAA SCITECH 2024 Forum;2024-01-04

3. Modeling Symmetric Coherent Mode Interactions in a Supersonic Rectangular Jet;AIAA Journal;2023-12-29

4. 3D Nonlinear Integral Technique Based on Linearized Euler Equations for the Prediction of Supersonic Rectangular Jet Noise Sources;AIAA SCITECH 2023 Forum;2023-01-19

5. Turbulent Statistics of a Hot, Overexpanded Rectangular Jet;Journal of Propulsion and Power;2022-05

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