Study of the Flow Structure in Supersonic Fluidic Element with Numerical Calculation Method
Author:
Affiliation:
1. Beijing Institute of Technology,School of Aerospace Engineering,Beijing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9849705/9849682/09849783.pdf?arnumber=9849783
Reference12 articles.
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3. Coupling of twin rectangular supersonic jets
4. Method of Testing of Dynamic Forces on Digital Jet Elements;mo;Journal of Beijing Institute of Technology,2002
5. Investigation of the Unsteady Flow for the Supersonic Jet Element;xu;Advanced Materials Research,2011
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