TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
e) Fluid Dynamics and Aerothermodynamics
Experimental Investigation of Effect of Rods Inserted into Supersonic Main Flow on Porous Cavity Flow
Nao KUNIYOSHIMinoru YAGAIsao TERUYAMasaaki ISHIKAWA
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2014 Volume 12 Issue ists29 Pages Pe_29-Pe_34

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Abstract

In this study, an experiment was performed to clarify the flow field, in which the rods were normally inserted into a main supersonic flow with a porous cavity. In the experiment, a porous cavity is attached to a bottom wall of a main duct. A thermal tuft probe was adopted to detect a vertical flow direction in the cavity to monitor the flow behavior in the cavity. The experiments show that the three rods aligned spanwise retard the downstream displacement of the starting shock wave. It also reveals that the interaction among the rods, the porous cavity, and the starting shock wave changes the flow in the cavity suggesting the strong circulation between the cavity and the main supersonic flow. Moreover, the frequency shift of the cavity flow from about 370Hz to 400Hz is confirmed during the displacement of the starting shock wave from upstream to downstream of the porous cavity.

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© 2014 The Japan Society for Aeronautical and Space Sciences
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