Parameter Effects of Spanwise-arrayed Cylindrical Roughness Elements on Transition in the Falkner-Skan-Cooke Boundary Layer-Reference-Cited by-同舟云学术

Parameter Effects of Spanwise-arrayed Cylindrical Roughness Elements on Transition in the Falkner-Skan-Cooke Boundary Layer

Published:2022 Issue:2 Volume:65 Page:84-94
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

ISHIDA Takahiro¹,TSUKAHARA Takahiro²,TOKUGAWA Naoko¹

Affiliation:

1. Aeronautical Technology Directorate, JAXA

2. Department of Mechanical Engineering, Tokyo University of Science

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/65/2/65_T-20-74/_pdf

Reference16 articles.

1. 1) Saric, W. S., Reed, H. L., and White, E. B.: Stability and Transition of Three-dimensional Boundary Layers, Annu. Rev. Fluid Mech., 35 (2003), pp. 413–440.

2. 2) Radeztsky, R. H., Reibert, M. S., and Saric, W. S.: Effect of Isolated Micron-Sized Roughness on Transition in Swept-wing Flows, AIAA J., 37 (1999), pp. 1370–1377.

3. 3) Braslow, A. L. and Knox, E. C.: Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-layer Transition at Mach Numbers from 0 to 5, NASA TN-4363, 1958.

4. 4) Ueno, M., Kohzai, T., and Koga, S.: Transonic Wind Tunnel Test of the NASA CRM (Volume 1), JAXA-RM-13-017E, 2014, http://id.nii.ac.jp/1696/00002496/

5. 5) Von Doenhoff, A. E. and Braslow, A. L.: The Effect of Distributed Roughness on Laminar Flow, Boundary Layer Control, 1 (1961), pp. 657–681.

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