Shock Tunnel Investigations On Hypersonic Separated Flows

Knowledge of flow separation is very essential for proper understanding of both external and internal aerothermodynamics of bodies. Because of unique flow features such as thick boundary layers, merged shock layers, strong entropy layers, flow separation in the flow field of bodies at hypersonic spe...

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Bibliographic Details
Main Author: Reddeppa, P
Other Authors: Jagadeesh, G
Language:en_US
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/2005/586