Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25

Micro jets are used in the present experimental study as an active control. Flow from converging nozzle to suddenly expanded circular duct of larger cross-sectional area than that of nozzle exit area were studied experimentally, focusing attention on the base pressure and the flow development in the...

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Main Authors: Ashfaq, Syed, Khan, Sher Afghan
Format: Article
Language:English
Published: International Journal of Engineering Science & Advanced Technology 2014
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Online Access:http://irep.iium.edu.my/49906/1/2014_JAN_FEB_IJESAT.pdf
http://irep.iium.edu.my/49906/
http://ijesat.org/Volumes/2014_Vol_04_Iss_01/IJESAT_2014_01_01_09.pdf
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
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spelling my.iium.irep.49906 http://irep.iium.edu.my/49906/ Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 Ashfaq, Syed Khan, Sher Afghan TL780 Rockets Micro jets are used in the present experimental study as an active control. Flow from converging nozzle to suddenly expanded circular duct of larger cross-sectional area than that of nozzle exit area were studied experimentally, focusing attention on the base pressure and the flow development in the duct. Mach number and nozzle pressure ratio are considered as the flow parameters. The geometrical parameters considered are the area ratio of the sudden expansion duct cross-section area to the nozzle exit area and the length to diameter ratio of the duct. To find the effect of micro jets as an active control on base pressure as well as on the flow field developed in the duct, the micro jets of 1 mm orifice diameter are used. They are located at 900 intervals along a pitch circle diameter 1.3 times the nozzle exit diameter. In this study, the area ratio considered is 6.25. The flow parameter, nozzle pressure ratio (NPR) used were from 1.5 to 3, in steps of 0.5 and experiments were conducted for NPR 1.5, 2.0, 2.5 and 3.0. The geometrical parameter, the length to diameter ratio of the enlarged duct was varied from 10 to 1, and tests were conducted for L/D 10, 8, 6, 5, 4, 3, 2 and 1. When the micro jets were activated they are found to influence the base region, taking the base suction to considerably higher values compared to that for without control case for most of the cases. From the present study it is found that as the NPR increases, the effect on base pressure is marginal for NPRs up to 2.5; however, at NPR 3 there is a sudden decrease in the base pressure. Further, it is found that the micro jets are very effective in controlling the base pressure and the active control in the form of micro jets does not disturb the flow field in the duct, however, wall pressure becomes oscillatory at NPR 3. International Journal of Engineering Science & Advanced Technology 2014-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/49906/1/2014_JAN_FEB_IJESAT.pdf Ashfaq, Syed and Khan, Sher Afghan (2014) Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25. International Journal of Engineering Science & Advanced Technology, 4 (1). pp. 49-60. ISSN 2250-3676 http://ijesat.org/Volumes/2014_Vol_04_Iss_01/IJESAT_2014_01_01_09.pdf
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 TL780 Rockets
spellingShingle TL780 Rockets
Ashfaq, Syed
Khan, Sher Afghan
Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
description Micro jets are used in the present experimental study as an active control. Flow from converging nozzle to suddenly expanded circular duct of larger cross-sectional area than that of nozzle exit area were studied experimentally, focusing attention on the base pressure and the flow development in the duct. Mach number and nozzle pressure ratio are considered as the flow parameters. The geometrical parameters considered are the area ratio of the sudden expansion duct cross-section area to the nozzle exit area and the length to diameter ratio of the duct. To find the effect of micro jets as an active control on base pressure as well as on the flow field developed in the duct, the micro jets of 1 mm orifice diameter are used. They are located at 900 intervals along a pitch circle diameter 1.3 times the nozzle exit diameter. In this study, the area ratio considered is 6.25. The flow parameter, nozzle pressure ratio (NPR) used were from 1.5 to 3, in steps of 0.5 and experiments were conducted for NPR 1.5, 2.0, 2.5 and 3.0. The geometrical parameter, the length to diameter ratio of the enlarged duct was varied from 10 to 1, and tests were conducted for L/D 10, 8, 6, 5, 4, 3, 2 and 1. When the micro jets were activated they are found to influence the base region, taking the base suction to considerably higher values compared to that for without control case for most of the cases. From the present study it is found that as the NPR increases, the effect on base pressure is marginal for NPRs up to 2.5; however, at NPR 3 there is a sudden decrease in the base pressure. Further, it is found that the micro jets are very effective in controlling the base pressure and the active control in the form of micro jets does not disturb the flow field in the duct, however, wall pressure becomes oscillatory at NPR 3.
format Article
author Ashfaq, Syed
Khan, Sher Afghan
author_facet Ashfaq, Syed
Khan, Sher Afghan
author_sort Ashfaq, Syed
title Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
title_short Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
title_full Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
title_fullStr Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
title_full_unstemmed Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
title_sort studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
publisher International Journal of Engineering Science & Advanced Technology
publishDate 2014
url http://irep.iium.edu.my/49906/1/2014_JAN_FEB_IJESAT.pdf
http://irep.iium.edu.my/49906/
http://ijesat.org/Volumes/2014_Vol_04_Iss_01/IJESAT_2014_01_01_09.pdf
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