Study on the characteristics of interaction flowfields induced by supersonic jet on a revolution body

The paper focuses on the triple jets interaction with a hypersonic external flow on a revolution body. The experimental model is a ogive-cylinder body with three supersonic nozzles, which are aligned along the flow direction. The freestream Mach numbers are 5 and 6. The spatial and surface flow char...

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Bibliographic Details

Published in:	Theoretical and Applied Mechanics Letters
Main Authors:	S.J. Luo, Z.Y. Ni, Y.F. Liu
Format:	Article
Language:	English
Published:	Elsevier 2017-11-01
Subjects:	Hypersonic flow Lateral jet interaction Wind tunnel Schlieren visualization Pressure
Online Access:	http://www.sciencedirect.com/science/article/pii/S2095034917301332