Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows

Base pressure becomes a decisive factor in governing the base drag of aerodynamic vehicles. While several experimental and numerical methods have already been used for base pressure analysis in suddenly expanded flows, their implementation is quite time consuming. Therefore, we must develop a progre...

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Autores principales: Jaimon Dennis Quadros, Sher Afghan Khan, Abdul Aabid, Mohammad Shohag Alam, Muneer Baig
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Lenguaje:EN
Publicado: MDPI AG 2021
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Acceso en línea:https://doaj.org/article/505c633c7e0048aea339d0e6f931deba
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spelling oai:doaj.org-article:505c633c7e0048aea339d0e6f931deba2021-11-25T15:57:10ZMachine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows10.3390/aerospace81103182226-4310https://doaj.org/article/505c633c7e0048aea339d0e6f931deba2021-10-01T00:00:00Zhttps://www.mdpi.com/2226-4310/8/11/318https://doaj.org/toc/2226-4310Base pressure becomes a decisive factor in governing the base drag of aerodynamic vehicles. While several experimental and numerical methods have already been used for base pressure analysis in suddenly expanded flows, their implementation is quite time consuming. Therefore, we must develop a progressive approach to determine base pressure (β). Furthermore, a direct consideration of the influence of flow and geometric parameters cannot be studied by using these methods. This study develops a platform for data-driven analysis of base pressure (β) prediction in suddenly expanded flows, in which the influence of flow and geometric parameters including Mach number (M), nozzle pressure ratio (η), area ratio (α), and length to diameter ratio (φ) have been studied. Three different machine learning (ML) models, namely, artificial neural networks (ANN), support vector machine (SVM), and random forest (RF), have been trained using a large amount of data developed from response equations. The response equations for base pressure (β) were created using the response surface methodology (RSM) approach. The predicted results are compared with the experimental results to validate the proposed platform. The results obtained from this work can be applied in the right way to maximize base pressure in rockets and missiles to minimize base drag.Jaimon Dennis QuadrosSher Afghan KhanAbdul AabidMohammad Shohag AlamMuneer BaigMDPI AGarticlebase pressuremachine learningartificial neural networkssupport vector machinerandom forestresponse surface methodologyMotor vehicles. Aeronautics. AstronauticsTL1-4050ENAerospace, Vol 8, Iss 318, p 318 (2021)
institution DOAJ
collection DOAJ
language EN
topic base pressure
machine learning
artificial neural networks
support vector machine
random forest
response surface methodology
Motor vehicles. Aeronautics. Astronautics
TL1-4050
spellingShingle base pressure
machine learning
artificial neural networks
support vector machine
random forest
response surface methodology
Motor vehicles. Aeronautics. Astronautics
TL1-4050
Jaimon Dennis Quadros
Sher Afghan Khan
Abdul Aabid
Mohammad Shohag Alam
Muneer Baig
Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
description Base pressure becomes a decisive factor in governing the base drag of aerodynamic vehicles. While several experimental and numerical methods have already been used for base pressure analysis in suddenly expanded flows, their implementation is quite time consuming. Therefore, we must develop a progressive approach to determine base pressure (β). Furthermore, a direct consideration of the influence of flow and geometric parameters cannot be studied by using these methods. This study develops a platform for data-driven analysis of base pressure (β) prediction in suddenly expanded flows, in which the influence of flow and geometric parameters including Mach number (M), nozzle pressure ratio (η), area ratio (α), and length to diameter ratio (φ) have been studied. Three different machine learning (ML) models, namely, artificial neural networks (ANN), support vector machine (SVM), and random forest (RF), have been trained using a large amount of data developed from response equations. The response equations for base pressure (β) were created using the response surface methodology (RSM) approach. The predicted results are compared with the experimental results to validate the proposed platform. The results obtained from this work can be applied in the right way to maximize base pressure in rockets and missiles to minimize base drag.
format article
author Jaimon Dennis Quadros
Sher Afghan Khan
Abdul Aabid
Mohammad Shohag Alam
Muneer Baig
author_facet Jaimon Dennis Quadros
Sher Afghan Khan
Abdul Aabid
Mohammad Shohag Alam
Muneer Baig
author_sort Jaimon Dennis Quadros
title Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
title_short Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
title_full Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
title_fullStr Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
title_full_unstemmed Machine Learning Applications in Modelling and Analysis of Base Pressure in Suddenly Expanded Flows
title_sort machine learning applications in modelling and analysis of base pressure in suddenly expanded flows
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/505c633c7e0048aea339d0e6f931deba
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AT abdulaabid machinelearningapplicationsinmodellingandanalysisofbasepressureinsuddenlyexpandedflows
AT mohammadshohagalam machinelearningapplicationsinmodellingandanalysisofbasepressureinsuddenlyexpandedflows
AT muneerbaig machinelearningapplicationsinmodellingandanalysisofbasepressureinsuddenlyexpandedflows
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