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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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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1724886638858862592 |