Estimation of Wind Tunnel Corrections Using Potential Models

The evaluation of the tunnel correction remains an actual problem, especially for the effect of tunnel walls. Even if the experimental campaign meets the basic similitude criteria (Mach, Reynolds etc.), the wall effect on the measured data is always present. Consequently, the flow correction due the...

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Main Authors: Ionut BUNESCU, Sterian DANAILA, Mihai-Victor PRICOP, Adrian DINA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2019-03-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/bunescu_danaila_pricop_dina_vol_11_iss_1.pdf
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spelling doaj-9227cc97512d483da7a246cdfb7b17872020-11-25T02:17:23ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282019-03-01111536010.13111/2066-8201.2019.11.1.4Estimation of Wind Tunnel Corrections Using Potential ModelsIonut BUNESCU0Sterian DANAILA1Mihai-Victor PRICOP2Adrian DINA3INCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, 061126 Bucharest, Romania, bunescu.ionut@incas.ro*“POLITEHNICA” University of Bucharest, Faculty of Aerospace Engineering, Department of Aerospace Sciences “Elie Carafoli”, Str. Polizu 1-7, sector 1, 011061 Bucharest, Romania, sterian.danaila@gmail.comINCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, 061126 Bucharest, Romania, pricop.victor@incas.ro, dina.adrian@incas.roINCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, 061126 Bucharest, Romania, dina.adrian@incas.roThe evaluation of the tunnel correction remains an actual problem, especially for the effect of tunnel walls. Even if the experimental campaign meets the basic similitude criteria (Mach, Reynolds etc.), the wall effect on the measured data is always present. Consequently, the flow correction due the limited by walls must be evaluated. Solid wall corrections refer to the aerodynamic interference between the experimental model and the walls of the wind tunnel. This interaction affects the measured forces and implicitly the angle of attack. Usually, these effects are introduced through semi-empirical correction factors which change the global measured forces. The present paper refers to the mathematical and numerical modeling of aerodynamic interferences between the experimental model and the solid walls based on the potential flow model. The main goal is to asses a method allowing an estimate of the corrections for each configuration with a minimum computational resource.http://bulletin.incas.ro/files/bunescu_danaila_pricop_dina_vol_11_iss_1.pdfsolid walls correctionswall interferencepanel methodsmethod of images
collection DOAJ
language English
format Article
sources DOAJ
author Ionut BUNESCU
Sterian DANAILA
Mihai-Victor PRICOP
Adrian DINA
spellingShingle Ionut BUNESCU
Sterian DANAILA
Mihai-Victor PRICOP
Adrian DINA
Estimation of Wind Tunnel Corrections Using Potential Models
INCAS Bulletin
solid walls corrections
wall interference
panel methods
method of images
author_facet Ionut BUNESCU
Sterian DANAILA
Mihai-Victor PRICOP
Adrian DINA
author_sort Ionut BUNESCU
title Estimation of Wind Tunnel Corrections Using Potential Models
title_short Estimation of Wind Tunnel Corrections Using Potential Models
title_full Estimation of Wind Tunnel Corrections Using Potential Models
title_fullStr Estimation of Wind Tunnel Corrections Using Potential Models
title_full_unstemmed Estimation of Wind Tunnel Corrections Using Potential Models
title_sort estimation of wind tunnel corrections using potential models
publisher National Institute for Aerospace Research “Elie Carafoli” - INCAS
series INCAS Bulletin
issn 2066-8201
2247-4528
publishDate 2019-03-01
description The evaluation of the tunnel correction remains an actual problem, especially for the effect of tunnel walls. Even if the experimental campaign meets the basic similitude criteria (Mach, Reynolds etc.), the wall effect on the measured data is always present. Consequently, the flow correction due the limited by walls must be evaluated. Solid wall corrections refer to the aerodynamic interference between the experimental model and the walls of the wind tunnel. This interaction affects the measured forces and implicitly the angle of attack. Usually, these effects are introduced through semi-empirical correction factors which change the global measured forces. The present paper refers to the mathematical and numerical modeling of aerodynamic interferences between the experimental model and the solid walls based on the potential flow model. The main goal is to asses a method allowing an estimate of the corrections for each configuration with a minimum computational resource.
topic solid walls corrections
wall interference
panel methods
method of images
url http://bulletin.incas.ro/files/bunescu_danaila_pricop_dina_vol_11_iss_1.pdf
work_keys_str_mv AT ionutbunescu estimationofwindtunnelcorrectionsusingpotentialmodels
AT steriandanaila estimationofwindtunnelcorrectionsusingpotentialmodels
AT mihaivictorpricop estimationofwindtunnelcorrectionsusingpotentialmodels
AT adriandina estimationofwindtunnelcorrectionsusingpotentialmodels
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