Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD
Sudden expansion of flow in supersonic flow regime has gained relevance in the recent pasts for a wide run of applications. A number of kinematic as well as geometric parameters have been significantly found to impact the base pressure created within the suddenly expanded stream. The current researc...
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Isfahan University of Technology
2020
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my.iium.irep.821682020-08-13T13:27:46Z http://irep.iium.edu.my/82168/ Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD Quadros, Jaimon Dennis Khan, Sher Afghan TJ Mechanical engineering and machinery TJ170 Mechanics applied to machinery. Dynamics Sudden expansion of flow in supersonic flow regime has gained relevance in the recent pasts for a wide run of applications. A number of kinematic as well as geometric parameters have been significantly found to impact the base pressure created within the suddenly expanded stream. The current research intends to create a predictive model for base pressure that is established in the abruptly extended stream. The artificial neural network (ANN) approach is being utilized for this purpose. The database utilized for training the network was assembled utilizing computational fluid dynamics (CFD). This was done by the design of experiments based L27 Orthogonal array. The three input parameters were Mach number (M), nozzle pressure ratio (NPR) and area ratio (AR) and base pressure was the output parameter. The CFD numerical demonstrate was approved by an experimental test rig that developed results for base pressure, and used a nozzle and sudden extended axissymmetric duct to do so. The ANN architecture comprised of three layers with eight neurons in the hidden layer. The algorithm for optimization was Levenberg-Marquardt. The ANN was able to successfully predict the base pressure with a regression coefficient R2 of less than 0.99 and RMSE=0.0032. The importance of input parameters influencing base pressure was estimated by using the ANN weight coefficients. Mach number obtained a relative importance of 47.16% claiming to be the most dominating factor. © Isfahan University of Technology. Isfahan University of Technology 2020-03 Article PeerReviewed application/pdf en http://irep.iium.edu.my/82168/1/82168_Prediction%20of%20base%20pressure.pdf application/pdf en http://irep.iium.edu.my/82168/2/82168_Prediction%20of%20base%20pressure_SCOPUS.pdf application/pdf en http://irep.iium.edu.my/82168/3/82168_Prediction%20of%20base%20pressure_WOS.pdf Quadros, Jaimon Dennis and Khan, Sher Afghan (2020) Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD. Journal of Applied Fluid Mechanics, 13 (2). pp. 499-511. ISSN 1735-3572 E-ISSN 1735-3645 http://jafmonline.net/web/guest/home?p_p_id=JournalArchive_WAR_JournalArchive_INSTANCE_nvhn&p_p_action=0&p_p_state=maximized&p_p_mode=view&p_p_col_id=column-2&p_p_col_pos=3&p_p_col_count=6&_JournalArchive_WAR_JournalArchive_INSTANCE_nvhn_form_page=main_form&selectedVolumeId=76&selectedIssueId=1005 10.29252/jafm.13.02.30049 |
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TJ Mechanical engineering and machinery TJ170 Mechanics applied to machinery. Dynamics Quadros, Jaimon Dennis Khan, Sher Afghan Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
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Sudden expansion of flow in supersonic flow regime has gained relevance in the recent pasts for a wide run of applications. A number of kinematic as well as geometric parameters have been significantly found to impact the base pressure created within the suddenly expanded stream. The current research intends to create a predictive model for base pressure that is established in the abruptly extended stream. The artificial neural network (ANN) approach is being utilized for this purpose. The database utilized for training the network was assembled utilizing computational fluid dynamics (CFD). This was done by the design of experiments based L27 Orthogonal array. The three input parameters were Mach number (M), nozzle pressure ratio (NPR) and area ratio (AR) and base pressure was the output parameter. The CFD numerical demonstrate was approved by an experimental test rig that developed results for base pressure, and used a nozzle and sudden extended axissymmetric duct to do so. The ANN architecture comprised of three layers with eight neurons in the hidden layer. The algorithm for optimization was Levenberg-Marquardt. The ANN was able to successfully predict the base pressure with a regression coefficient R2 of less than 0.99 and RMSE=0.0032. The importance of input parameters influencing base pressure was estimated by using the ANN weight coefficients. Mach number obtained a relative importance of 47.16% claiming to be the most dominating factor. © Isfahan University of Technology. |
format |
Article |
author |
Quadros, Jaimon Dennis Khan, Sher Afghan |
author_facet |
Quadros, Jaimon Dennis Khan, Sher Afghan |
author_sort |
Quadros, Jaimon Dennis |
title |
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
title_short |
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
title_full |
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
title_fullStr |
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
title_full_unstemmed |
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD |
title_sort |
prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ann and cfd |
publisher |
Isfahan University of Technology |
publishDate |
2020 |
url |
http://irep.iium.edu.my/82168/1/82168_Prediction%20of%20base%20pressure.pdf http://irep.iium.edu.my/82168/2/82168_Prediction%20of%20base%20pressure_SCOPUS.pdf http://irep.iium.edu.my/82168/3/82168_Prediction%20of%20base%20pressure_WOS.pdf http://irep.iium.edu.my/82168/ http://jafmonline.net/web/guest/home?p_p_id=JournalArchive_WAR_JournalArchive_INSTANCE_nvhn&p_p_action=0&p_p_state=maximized&p_p_mode=view&p_p_col_id=column-2&p_p_col_pos=3&p_p_col_count=6&_JournalArchive_WAR_JournalArchive_INSTANCE_nvhn_form_page=main_form&selectedVolumeId=76&selectedIssueId=1005 |
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1675327180472582144 |
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13.160551 |