Numerical Study of Supersonic Jet Noise Emanating from an F404 Nozzle at Model Scale-Reference-Cited by-同舟云学术

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Numerical Study of Supersonic Jet Noise Emanating from an F404 Nozzle at Model Scale

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Liu Junhui¹,Ramamurti Ravi¹

Affiliation:

1. Naval Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0807

Reference28 articles.

1. https://www.benefits.va.gov/REPORTS/abr/ABR-Compensation-FY15-05092016.pdf

2. Jet Noise Simulations for Complex Nozzle Geometries

3. Liu, J., Corrigan, A., Kailasanath, K., Pablo, M., Heeb, N., and Gutmark. E. "Computational Study of Shock-Associated Noise Characteristics Using LES", NRL Memorandum Report, NRL/MR/6040-14-9560.

Cited by 14 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. Acoustical Holography and Coherence-Based Noise Source Characterization of an Installed F404 Engine;AIAA Journal;2024-06

2. Data Driven Machine Learning Models for Accelerating Jet Engine Noise Predictions;AIAA SCITECH 2024 Forum;2024-01-04

3. Noise Reduction by Lowering the Jet Mach Number at Fixed Thrust and Mass Flow;AIAA AVIATION 2023 Forum;2023-06-08

4. High-Order Accurate Numerical Simulation of Supersonic Flow Using RANS and LES Guided by Turbulence Anisotropy;Fluids;2022-12-14

5. Acoustic Source Characterization of an Installed GE F404 Engine Using Near-field Acoustical Holography;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

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