Investigations of influence of Free Stream Turbulence and Acoustic Disturbances on the Laminar-Turbulent Transition on LV6 Airfoil and Swept Wing Models-Reference-Cited by-同舟云学术

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Investigations of influence of Free Stream Turbulence and Acoustic Disturbances on the Laminar-Turbulent Transition on LV6 Airfoil and Swept Wing Models

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Chernyshev Sergey¹,Ivanov Alexander¹,Kiselev Andrey¹,Kuzminsky Vladimir¹,Sboev Dmitry¹,Zhigulev Sergey¹

Affiliation:

1. TsAGI

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-210

Reference31 articles.

1. 1Bieler, H., Abbas, A., Chiaramonte, J.Y. and Sawyers, D. "Flow control for aircraft performance enhancements. Overview of Airbus - Universitycooperation,"AIAA paper, No. 2006-3692,2006.

2. AIRCRAFT LAMINAR FLOW CONTROL

3. 3Aeronauticsresearch2003-2006projects,Projectsynopses,EuropeanCommission,Belgium,Luxembourg,2006,Vol.1.

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2. Role of Freestream Slow Acoustic Waves in a Hypersonic Three-Dimensional Boundary Layer;AIAA Journal;2018-09

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

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