Numerical simulation of laminar-turbulent transition in a supersonic boundary layer under the action of acoustic disturbances-Reference-Cited by-同舟云学术

Numerical simulation of laminar-turbulent transition in a supersonic boundary layer under the action of acoustic disturbances

Published:2024-03 Issue: Volume:220 Page:124895
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Egorov I.V.,Fedorov A.V.^ORCID,Palchekovskaya N.V.

Funder

Russian Science Foundation

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference29 articles.

1. Receptivity of a hypersonic flow over a blunt wedge to a slow acoustic wave;Chen;Phys. Fluids,2021

2. Acoustic receptivity of high-speed boundary layers on a flat plate at angles of attack;Fedorov;Theor. Comput. Fluid Dyn.,2022

3. M. Malik, T. Zang and D. Bushnell, Boundary layer transition in hypersonic flows, AIAA Paper no. 90-5232 (1990).

4. D. Arnal, Transition Prediction in Industrial Applications, Transition, Turbulence and Combustion Modeling, ERCOFTAC Series, Hani A., Alfredsson P.H., Johansson A.V. and Henningson D.S. eds., Kluwer Academic Publishers (1998).

5. Transition and Laminar Instability, NASA-CP-153203;Mack,1977

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