Shock-Induced Separation Control by Using Nanosecond Pulsed SDBD Plasma Actuators (AIAA 2014-2368)
Conference; 7th, Flow control; 7th AIAA flow control conference 2014; Atlanta, Georgia, USA, 16-20 June 2014 : held at the AIAA aviation forum 2014 ; 2014 ; Atlanta, GA
2014-01-01
13 pages
Includes bibliographical references and index
Conference paper
English
AIAA , Flow control , Aviation , Aeronautics
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
An Empirical Model of Nanosecond Pulsed SDBD Actuators for Separation Control
British Library Conference Proceedings | 2013
|Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators AIAA Paper
British Library Conference Proceedings | 2007
|Study of Shock and Induced Flow Dynamics by Pulsed Nanosecond DBD Plasma Actuators (AIAA 2014-0402)
British Library Conference Proceedings | 2014
|