Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers

The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers. The analysis is made for variation in the nozzle pressure ratio (NPR), length to diamet...

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Main Authors: Afzal, Asif, Khan, Sher Afghan, Islam, Md. Tariqul, Jilte, R. D., Khan, Ambareen, Soudagar, Manzoore Elahi M
Format: Article
Language:English
English
English
Published: AIP Publishing 2020
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Online Access:http://irep.iium.edu.my/83245/1/83245_Investigation%20and%20back-propagation%20modeling_ft.pdf
http://irep.iium.edu.my/83245/7/83245_Investigation%20and%20back-propagation%20modeling_SCOPUS.pdf
http://irep.iium.edu.my/83245/8/83245_Investigation%20and%20back-propagation%20modeling_WOS.pdf
http://irep.iium.edu.my/83245/
https://aip.scitation.org/doi/10.1063/5.0022015
https://doi.org/10.1063/5.0022015
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Institution: Universiti Islam Antarabangsa Malaysia
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spelling my.iium.irep.832452020-11-23T06:45:11Z http://irep.iium.edu.my/83245/ Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers Afzal, Asif Khan, Sher Afghan Islam, Md. Tariqul Jilte, R. D. Khan, Ambareen Soudagar, Manzoore Elahi M TL780 Rockets The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers. The analysis is made for variation in the nozzle pressure ratio (NPR), length to diameter ratio, and area ratio. The effect of active micro-jets on the base and wall pressure is assessed. The data visualization of the huge experimental data generated is performed using heat maps. For the first time, six back-propagation neural network models (BPMs) are developed based on input and output possibilities to predict the pressure in high-speed flows. The experimental analysis revealed that depending upon the type of expansion, the base pressure changes. A jet of air blown at the base using micro-jets is found to be effective in increasing the base pressure during the under-expansion regime, while the wall pressure remains unaffected. The data visualization provided an insight into the highest impact on the base pressure by the NPR. The six BPMs with two hidden layers having four neurons per layer are found to be most suitable for the regression analysis. BPM 5 and BPM 6 accurately predict the highly non-linear data of the base and wall pressure. AIP Publishing 2020-09-21 Article PeerReviewed application/pdf en http://irep.iium.edu.my/83245/1/83245_Investigation%20and%20back-propagation%20modeling_ft.pdf application/pdf en http://irep.iium.edu.my/83245/7/83245_Investigation%20and%20back-propagation%20modeling_SCOPUS.pdf application/pdf en http://irep.iium.edu.my/83245/8/83245_Investigation%20and%20back-propagation%20modeling_WOS.pdf Afzal, Asif and Khan, Sher Afghan and Islam, Md. Tariqul and Jilte, R. D. and Khan, Ambareen and Soudagar, Manzoore Elahi M (2020) Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers. Physics of Fluids, 32 (9). pp. 1-18. ISSN 1070-6631 E-ISSN 1089-7666 https://aip.scitation.org/doi/10.1063/5.0022015 https://doi.org/10.1063/5.0022015
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
English
English
topic TL780 Rockets
spellingShingle TL780 Rockets
Afzal, Asif
Khan, Sher Afghan
Islam, Md. Tariqul
Jilte, R. D.
Khan, Ambareen
Soudagar, Manzoore Elahi M
Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
description The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers. The analysis is made for variation in the nozzle pressure ratio (NPR), length to diameter ratio, and area ratio. The effect of active micro-jets on the base and wall pressure is assessed. The data visualization of the huge experimental data generated is performed using heat maps. For the first time, six back-propagation neural network models (BPMs) are developed based on input and output possibilities to predict the pressure in high-speed flows. The experimental analysis revealed that depending upon the type of expansion, the base pressure changes. A jet of air blown at the base using micro-jets is found to be effective in increasing the base pressure during the under-expansion regime, while the wall pressure remains unaffected. The data visualization provided an insight into the highest impact on the base pressure by the NPR. The six BPMs with two hidden layers having four neurons per layer are found to be most suitable for the regression analysis. BPM 5 and BPM 6 accurately predict the highly non-linear data of the base and wall pressure.
format Article
author Afzal, Asif
Khan, Sher Afghan
Islam, Md. Tariqul
Jilte, R. D.
Khan, Ambareen
Soudagar, Manzoore Elahi M
author_facet Afzal, Asif
Khan, Sher Afghan
Islam, Md. Tariqul
Jilte, R. D.
Khan, Ambareen
Soudagar, Manzoore Elahi M
author_sort Afzal, Asif
title Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
title_short Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
title_full Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
title_fullStr Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
title_full_unstemmed Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
title_sort investigation and back-propagation modeling of base pressure at sonic and supersonic mach numbers
publisher AIP Publishing
publishDate 2020
url http://irep.iium.edu.my/83245/1/83245_Investigation%20and%20back-propagation%20modeling_ft.pdf
http://irep.iium.edu.my/83245/7/83245_Investigation%20and%20back-propagation%20modeling_SCOPUS.pdf
http://irep.iium.edu.my/83245/8/83245_Investigation%20and%20back-propagation%20modeling_WOS.pdf
http://irep.iium.edu.my/83245/
https://aip.scitation.org/doi/10.1063/5.0022015
https://doi.org/10.1063/5.0022015
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