Analysis of flow field across blunt fin with dimples — Experimentation

Author

Sekaran, M.K.S. ; Naik, B.A.

Author_Institution

Vel Tech Dr RR & Dr SR Tech. Univ., Avadi, India

Volume

3

fYear

2011

fDate

12-14 Aug. 2011

Firstpage

1185

Lastpage

1188

Abstract

Experimental studies are made on the hemi - cylindrically blunted fins for Mach 2.2 to examine the effect of dimples on shock wave / boundary layer interaction. Flow field details around hemi - cylindrically blunted fin has been captured using oil flow visualization, measurements of static and total pressures and lambda shock has been captured by shadowgraphy technique. Studies show that the configuration indicate nonstart without any dimples whereas startup is observed with adoption of dimples on the leading edge of blunt fin. Studies have been also made by varying the number of holes, diameter of holes and height of blunt fins. In addition, improvement in reduction of separation region has been observed.

Keywords

Mach number; boundary layers; flow visualisation; shapes (structures); shock waves; Mach 2.2; blunt fin; dimples; flow field analysis; hemicylindrically blunted fins; lambda shock; oil flow measurements; oil flow visualization; separation region; shadowgraphy technique; shock wave-boundary layer interaction; startup; Electric shock; Mirrors; Shock waves; Silicon; Surface waves; Vehicles; Visualization;

fLanguage

English

Publisher

ieee

Conference_Titel

Electronic and Mechanical Engineering and Information Technology (EMEIT), 2011 International Conference on

Conference_Location

Harbin, Heilongjiang, China

Print_ISBN

978-1-61284-087-1

Type

conf

DOI

10.1109/EMEIT.2011.6023306

Filename

6023306