Numerical and Experimental Analysis of Three-Dimensional Boundary-Layer Transition Induced by Isolated Cylindrical Roughness Elements-Reference-Cited by-同舟云学术

Numerical and Experimental Analysis of Three-Dimensional Boundary-Layer Transition Induced by Isolated Cylindrical Roughness Elements

Published:2022-07-06 Issue:4 Volume:23 Page:649-659
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Ishida Takahiro,Ohira Keisuke,Hosoi Rio,Tokugawa Naoko,Tsukahara Takahiro

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-022-00485-0.pdf

Reference29 articles.

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3. Saric WS, Reed HL, White EB (2003) Stability and transition of three-dimensional boundary layers. Annu Rev Fluid Mech 35(1):413–440. https://doi.org/10.1146/annurev.fluid.35.101101.161045

4. Ueno M, Kohzai M, Koga S, Kato H, Nakakita K, Sudani N, Nakamura Y (2015) Normalization of wind-tunnel data for NASA common research model. J Aircr 52(5):1535–1549. https://doi.org/10.2514/1.C032989

5. Braslow AL, Knox EC (1958) Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5. NACA TN-4363

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