A Study on the Separation Length of Shock WaveTurbulent Boundary Layer Interaction
Joint Authors
Zhou, Yong-yi
Zhao, Yi-long
Zhao, Yu-xin
Source
International Journal of Aerospace Engineering
Issue
Vol. 2019, Issue 2019 (31 Dec. 2019), pp.1-10, 10 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2019-10-20
Country of Publication
Egypt
No. of Pages
10
Abstract EN
The separation length of shock wave/boundary layer interaction (SWBLI) was studied by a numerical method, which was validated by experimental results.
The computational domain was two-dimensional (2-D).
The flow field was an incident oblique shock interacting with a turbulent boundary layer on a flat adiabatic plate.
According to the simulation data, the dependency of the separation length on the relevant flow parameters, such as the incident shock strength, Reynolds number, and Mach number, was analyzed in the range of 2≤M≤7.
Based on the relations with the flow parameters, two models of the separation length at low and high Mach numbers were proposed, respectively, which can be used to predict the extent of the separation in the SWBLI.
American Psychological Association (APA)
Zhou, Yong-yi& Zhao, Yi-long& Zhao, Yu-xin. 2019. A Study on the Separation Length of Shock WaveTurbulent Boundary Layer Interaction. International Journal of Aerospace Engineering،Vol. 2019, no. 2019, pp.1-10.
https://search.emarefa.net/detail/BIM-1157038
Modern Language Association (MLA)
Zhou, Yong-yi…[et al.]. A Study on the Separation Length of Shock WaveTurbulent Boundary Layer Interaction. International Journal of Aerospace Engineering No. 2019 (2019), pp.1-10.
https://search.emarefa.net/detail/BIM-1157038
American Medical Association (AMA)
Zhou, Yong-yi& Zhao, Yi-long& Zhao, Yu-xin. A Study on the Separation Length of Shock WaveTurbulent Boundary Layer Interaction. International Journal of Aerospace Engineering. 2019. Vol. 2019, no. 2019, pp.1-10.
https://search.emarefa.net/detail/BIM-1157038
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1157038