Plasma-Based Flow Control for Delay of Excrescence-Generated Transition-Reference-Cited by-同舟云学术

Plasma-Based Flow Control for Delay of Excrescence-Generated Transition

Published:2015-06 Issue:6 Volume:53 Page:1455-1467
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rizzetta Donald P.¹,Visbal Miguel R.¹

Affiliation:

1. Aerodynamic Technology Branch, U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7512

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053289

Reference41 articles.

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2. BraslowA. L. “The Effect of Distributed Surface Roughness on Boundary-Layer Transition,” AGARD Rept. 254, NATO, Jan. 1960.

3. DrakeA.WestphalR. V.ZunigaF. A.KennellyR. A.KogaD. J. “Wing Leading Edge Joint Laminar Flow Tests,” NASA TM-4762, March 1997.

4. DrakeA.BenderA. M.SolomomW. D.VavraA. J. “Prediction of Manufacturing Tolerances for Laminar Flow,” U.S. Air Force Research Lab. TR AFRL-VA-WP-TR-2005-3060, Wright–Patterson AFB, OH, June 2005.

5. BenderA. M.DrakeA. “Manufacturing Tolerances for Laminar Flow,” U.S. Air Force Research Lab. TR AFRL-VA-WP-TR-2007-3086, Wright–Patterson AFB, OH, Sept. 2006.

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