Effect of level of expansion and inertia level in a suddenly expanded flow

An experimental study has been carried out to assess the effectiveness of the active control in the form of micro jets to control the base pressure in a suddenly expanded axi-symmetric duct. Four micro jets of 1mm orifice diameter located at 90 intervals along a pitch circle diameter of 1.3 times t...

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Main Authors: Chaudhary, Zakir Ilahi, Shinde, V.B, Ashfaq, Syed, Khan, Sher Afghan
Format: Conference or Workshop Item
Language:English
Published: 2015
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Online Access:http://irep.iium.edu.my/46657/1/46657.pdf
http://irep.iium.edu.my/46657/
http://www.ums.edu.my/upbmv2/index.php/en/journal/intro
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
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spelling my.iium.irep.466572016-03-30T05:49:57Z http://irep.iium.edu.my/46657/ Effect of level of expansion and inertia level in a suddenly expanded flow Chaudhary, Zakir Ilahi Shinde, V.B Ashfaq, Syed Khan, Sher Afghan TL500 Aeronautics TL780 Rockets TL787 Astronautics An experimental study has been carried out to assess the effectiveness of the active control in the form of micro jets to control the base pressure in a suddenly expanded axi-symmetric duct. Four micro jets of 1mm orifice diameter located at 90 intervals along a pitch circle diameter of 1.3 times the nozzle outlet diameter in the base region are employed as active controls. The Mach numbers of the present study are 2.5 and 3.0. The jets are expanded suddenly into an axi-symmetric circular tube with four cross-sectional area 2.56, 3.24, 4.84 and 6.25 times that of nozzle exit area. The Length to Diameter ratio of the suddenly expanded duct is varied from 10 to 1 and experiments are conducted for Nozzle Pressure Ratio (NPR) from 3 to 11. Since the jets remain over expanded for all the NPRs of the present study, even though, with increase in the NPR, the level of over expansion will decrease. It is well known that for over expanded nozzles an oblique shock will be formed at the nozzle lip, which in turn will result in the increase of the base pressure once it passes through the shock wave. From the results it is observed that for the NPRs 3 and 5 there is no appreciable gain in the base pressure, and hence, control employed in the form of micro jets is not effective, however, at NPR 7, 9, and 11 there is remarkable change in the base pressure values. This clearly indicates that the level of expansion plays a significant role to decide on the value of the base pressure and the control effectiveness of the micro jets. It is found that the micro jets can serve as an effective controller of base pressure in a suddenly expanded duct. The micro jets do not adversely influence the wall pressure flow field in the enlarge duct. 2015 Conference or Workshop Item REM application/pdf en http://irep.iium.edu.my/46657/1/46657.pdf Chaudhary, Zakir Ilahi and Shinde, V.B and Ashfaq, Syed and Khan, Sher Afghan (2015) Effect of level of expansion and inertia level in a suddenly expanded flow. In: International Conference on Mechanical Engineering & Advanced Material (ICME-AM2015), 3rd-4th Dec. 2015, Kota Kinabalu, Sabah. http://www.ums.edu.my/upbmv2/index.php/en/journal/intro
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
topic TL500 Aeronautics
TL780 Rockets
TL787 Astronautics
spellingShingle TL500 Aeronautics
TL780 Rockets
TL787 Astronautics
Chaudhary, Zakir Ilahi
Shinde, V.B
Ashfaq, Syed
Khan, Sher Afghan
Effect of level of expansion and inertia level in a suddenly expanded flow
description An experimental study has been carried out to assess the effectiveness of the active control in the form of micro jets to control the base pressure in a suddenly expanded axi-symmetric duct. Four micro jets of 1mm orifice diameter located at 90 intervals along a pitch circle diameter of 1.3 times the nozzle outlet diameter in the base region are employed as active controls. The Mach numbers of the present study are 2.5 and 3.0. The jets are expanded suddenly into an axi-symmetric circular tube with four cross-sectional area 2.56, 3.24, 4.84 and 6.25 times that of nozzle exit area. The Length to Diameter ratio of the suddenly expanded duct is varied from 10 to 1 and experiments are conducted for Nozzle Pressure Ratio (NPR) from 3 to 11. Since the jets remain over expanded for all the NPRs of the present study, even though, with increase in the NPR, the level of over expansion will decrease. It is well known that for over expanded nozzles an oblique shock will be formed at the nozzle lip, which in turn will result in the increase of the base pressure once it passes through the shock wave. From the results it is observed that for the NPRs 3 and 5 there is no appreciable gain in the base pressure, and hence, control employed in the form of micro jets is not effective, however, at NPR 7, 9, and 11 there is remarkable change in the base pressure values. This clearly indicates that the level of expansion plays a significant role to decide on the value of the base pressure and the control effectiveness of the micro jets. It is found that the micro jets can serve as an effective controller of base pressure in a suddenly expanded duct. The micro jets do not adversely influence the wall pressure flow field in the enlarge duct.
format Conference or Workshop Item
author Chaudhary, Zakir Ilahi
Shinde, V.B
Ashfaq, Syed
Khan, Sher Afghan
author_facet Chaudhary, Zakir Ilahi
Shinde, V.B
Ashfaq, Syed
Khan, Sher Afghan
author_sort Chaudhary, Zakir Ilahi
title Effect of level of expansion and inertia level in a suddenly expanded flow
title_short Effect of level of expansion and inertia level in a suddenly expanded flow
title_full Effect of level of expansion and inertia level in a suddenly expanded flow
title_fullStr Effect of level of expansion and inertia level in a suddenly expanded flow
title_full_unstemmed Effect of level of expansion and inertia level in a suddenly expanded flow
title_sort effect of level of expansion and inertia level in a suddenly expanded flow
publishDate 2015
url http://irep.iium.edu.my/46657/1/46657.pdf
http://irep.iium.edu.my/46657/
http://www.ums.edu.my/upbmv2/index.php/en/journal/intro
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