Effect of Nozzle Inflow Conditions on Shock-Cell Structure and Noise in Overexpanded Jets-Reference-Cited by-同舟云学术

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Effect of Nozzle Inflow Conditions on Shock-Cell Structure and Noise in Overexpanded Jets

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
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Author:

Liu Junhui¹,Corrigan Andrew T.¹,Johnson Ryan F.¹,Ramamurti Ravi¹

Affiliation:

1. Naval Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference33 articles.

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

2. Liu, J.; Corrigan, A.; Kailasanath, K.; and Gutmark; E. "Impact of Chevrons on Noise Source Characteristics In Imperfectly ExpandedJetFlows",21stAIAA/CEAS AeroacousticsConference, AIAA 2015-2835.

3. Liu, J., Corrigan, A.,Kailasanath,K., Pablo,M., Heeb, N., and Gutmark. E. "Computational Studyof Shock-AssociatedNoise CharacteristicsUsingLES",NRLMemorandumReport, NRL/MR/6040-14-9560.

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1. Initial boundary layer state of typical model-scale jet nozzles and its impact on noise;International Journal of Aeroacoustics;2023-09

2. Pressure fluctuations due to ‘trapped waves’ in the initial region of compressible jets;Journal of Fluid Mechanics;2021-11-29

3. Noise Characteristics of Low Aspect Ratio Supersonic Twin Jet Configuration;AIAA Scitech 2020 Forum;2020-01-05

4. Modelling of jet noise: a perspective from large-eddy simulations;Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences;2019-10-14

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