Electrogasdynamic laminar flow control on a swept wing

Authors

Keywords

Swept wing, Compressible boundary layer, Cross-flow-type instability, Dielectric barrier discharge actuator

Journal

AEROSPACE SCIENCE AND TECHNOLOGY

Volume 59, Issue -, Pages 155-161

Publisher

Elsevier BV

Online

2016-10-22

DOI

10.1016/j.ast.2016.10.019

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