Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators
Author:
Funder
the National Key R&D Program of China
the Chinese Scholarship Council
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2000025.pdf
Reference41 articles.
1. Adamovich IV, 2010. Plasma dynamics and flow control applications. In: Blockley R, Shyy W (Eds.), Encyclopedia of Aerospace Engineering. John Wiley & Sons, Chichester, UK, p.1–9. https://doi.org/10.1002/9780470686652.eae042
2. Atkinson MD, Poggie J, Camberos JA, 2012. Control of separated flow in a reflected shock interaction using a magnetically-accelerated surface discharge. Physics of Fluids, 24(12):126102. https://doi.org/10.1063/1.4772197
3. Babinsky H, Harvey JK, 2011. Shock Wave-boundary-layer Interactions. Cambridge University Press, Cambridge, UK, p.28–36.
4. Babinsky H, Li Y, Ford CWP, 2009. Microramp control of supersonic oblique shock-wave/boundary-layer interactions. AIAA Journal, 47(3):668–675. https://doi.org/10.2514/1.38022
5. Bisek N, Poggie J, 2013. Large-eddy simulations of separated supersonic flow with plasma control. Proceedings of the 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. https://doi.org/10.2514/6.2013-528
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