Study on transition to turbulence of rotating-disk boundary layer in a rotor-stator cavity with temperature gradient-Reference-Cited by-同舟云学术

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Study on transition to turbulence of rotating-disk boundary layer in a rotor-stator cavity with temperature gradient

Published:2024-05-15 Issue:5 Volume:9 Page:
ISSN:2469-990X
Container-title:Physical Review Fluids
language:en
Short-container-title:Phys. Rev. Fluids

Author:

Du Qiang¹^ORCID,Xie Yaguang¹,Xie Lei¹,Wang Ruonan²^ORCID

Affiliation:

1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, 100190 Beijing, China; Key Lab of Light-duty Gas-turbine, Chinese Academy of Sciences, 100190 Beijing, China; and University of Chinese Academy of Sciences, 100049 Beijing, China

2. Faculty of Engineering and Physical Sciences, University of Surrey, Guildford, GU2 7XH, United Kingdom

Funder

National Outstanding Youth Science Fund Project of National Natural Science Foundation of China

National Science and Technology Major Project

Sichuan Science and Technology Program

Publisher

American Physical Society (APS)

Link

http://harvest.aps.org/v2/journals/articles/10.1103/PhysRevFluids.9.053908/fulltext

Reference41 articles.

1. Über laminare und turbulente Reibung

2. Flows Over Rotating Disks and Cones

3. NOTE ON A CLASS OF SOLUTIONS OF THE NAVIER-STOKES EQUATIONS REPRESENTING STEADY ROTATIONALLY-SYMMETRIC FLOW

4. Laminar, Transitional, and Turbulent Flows in Rotor-Stator Cavities

5. Instabilities and routes to turbulence in rotating disc boundary layers and cavities

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