Review of swept-wing transition-Reference-Cited by-同舟云学术

Review of swept-wing transition

Published:1997-06-29 Issue: Volume: Page:
ISSN:
Container-title:28th Fluid Dynamics Conference
language:
Short-container-title:

Author:

Reibert Mark¹,Saric William¹,Reibert Mark¹,Saric William¹

Affiliation:

1. Arizona State Univ., Tempe

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1816

Reference59 articles.

1. Arnal, D. 1984.Description and prediction oftransition in two-dimensional incompressible flow. In Special Course on Stability and Transition of Laminar Flows, AGARD R-709.

2. Arnal, D. 1986. Three-dimensional boundary layers: Laminar-turbulent transition. In Special Course on Calculation of Three-Dimensional Boundary Layers with Separation, AGARD R-741.

3. Arnal, D., G. Casalis, and J. C. Juillen. 1990. Experimental and theoretical analysis of natural transition on infinite swept wing. In Laminar-Turbulent Transition (eds.D.Arnal and R. Michel), vol.3, pp.311-325. Berlin: Springer-Verlag. ISBN 3-540-52196-8.

Cited by 17 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. Experimental and Numerical Simulation Research on Boundary Layer Transition Front over a Swept Wing at M = 6;Fluid Dynamics;2021-05

2. Supersonic Crossflow Transition Control in Ground and Flight Tests;AIAA Scitech 2019 Forum;2019-01-06

3. Free-stream turbulence and the development of cross-flow disturbances;Journal of Fluid Mechanics;2013-10-24

4. Stability analysis: an experimental study of stationary crossflow instability for swept wing boundary layer;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

5. Direct Numerical Simulation of Discrete Roughness on a Swept-Wing Leading Edge;AIAA Journal;2010-11