Surface Step Effects on Boundary-Layer Transition Dominated by Tollmien–Schlichting Instability-Reference-Cited by-同舟云学术

Surface Step Effects on Boundary-Layer Transition Dominated by Tollmien–Schlichting Instability

Published:2020-07 Issue:7 Volume:58 Page:2943-2950
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Crouch J. D.¹,Kosorygin V. S.²

Affiliation:

1. The Boeing Company, Seattle, Washington 98124-2207

2. Siberian Branch Russian Academy of Sciences, 630090, Novosibirsk, Russia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference31 articles.

1. Boundary-Layer Transition Prediction for Laminar Flow Control (Invited)

2. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Co. Rept. ES26388, El Segundo, CA, 1956.

3. Van IngenJ. L. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Univ. of Tech., Rept. UTH1-74, Delft, The Netherlands, 1956.

4. TaniI.HamaR.MituisiS. “On the Permissible Roughness in the Laminar Boundary Layer,” Aeronautical Research Inst., Tokyo Imperial Univ. Rept. 1999, Tokyo, 1940.

Cited by 23 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Mitigation of Roughness-Induced Boundary-Layer Transition on Airfoils Using Shielding Strips;AIAA Journal;2024-07

2. Analysis of the Instability of Two-Dimensional Modes in Gaps;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

3. Bi-global stability of supersonic backward-facing step flow;Journal of Fluid Mechanics;2024-02-25

4. Computation of the Evolution of Tollmien–Schlichting Waves Based on Global Stability Analysis;Mathematical Models and Computer Simulations;2024-02

5. Influence of deep gaps on laminar–turbulent transition in two-dimensional boundary layers at subsonic Mach numbers;Experiments in Fluids;2023-10-28