Flow transition to turbulence and induced acoustics at Mach 6-Reference-Cited by-同舟云学术

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Flow transition to turbulence and induced acoustics at Mach 6

Published:2021-07 Issue:7 Volume:33 Page:076112
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Drikakis Dimitris¹^ORCID,Ritos Konstantinos²^ORCID,Spottswood S. Michael³,Riley Zachary B.⁴

Affiliation:

1. University of Nicosia, Nicosia CY-2417, Cyprus

2. Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow G1 1XJ, United Kingdom

3. Air Force Research Laboratory, Wright Patterson AFB, Dayton, Ohio 45433-7402, USA

4. ARCTOS Technology Solutions, LLC., Dayton, Ohio 45432, USA

Funder

European Office of Aerospace Research and Development

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

https://aip.scitation.org/doi/am-pdf/10.1063/5.0054345

Reference72 articles.

1. Wall pressure fluctuations in attached boundary-layer flow

2. Surface-pressure fluctuations induced by boundary-layer flow at finite Mach number

3. ‘Inactive’ motion and pressure fluctuations in turbulent boundary layers

4. Spectral features of wall pressure fluctuations beneath turbulent boundary layers

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