Evaluation of Vortex Generators for Separation Control in a Transcritical Cylinder Flow-Reference-Cited by-同舟云学术

Evaluation of Vortex Generators for Separation Control in a Transcritical Cylinder Flow

Published:2015-10 Issue:10 Volume:53 Page:2967-2977
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Shur Michael L.¹,Strelets Michael K.¹,Travin Andrey K.¹,Spalart Philippe R.²

Affiliation:

1. Laboratory of Computational Aeroacoustics and Turbulence; New Technologies and Services, St. Petersburg State Polytechnic University, 195220 St. Petersburg, Russia

2. Flight Sciences, Boeing Commercial Airplanes, The Boeing Company, Seattle, Washington 98124

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053851

Reference24 articles.

1. Review of research on low-profile vortex generators to control boundary-layer separation

2. Drag of a Circular Cylinder with Vortex Generators

3. The Influence of Vortex Generators on the Drag and Heat Transfer From a Circular Cylinder Normal to an Airstream

4. An experimental investigation into the effect of vortex generators on the near-wake flow of a circular cylinder

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