Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel

Wind tunnels usually use long cantilever stings to support aerodynamic models in order to reduce support system flow interference on experimental data. However, such support systems are a potential source of vibration problems which limit the test envelope and affect data quality due to the inherent...

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Main Authors: Jinjin Chen, Xing Shen, Fanfan Tu, Ehtesham Mustafa Qureshi
Format: Article
Language:English
Published: Hindawi Limited 2014-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2014/524351
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spelling doaj-88e22d728d8a4b8bbe901d9de03a89562020-11-24T23:20:09ZengHindawi LimitedShock and Vibration1070-96221875-92032014-01-01201410.1155/2014/524351524351Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind TunnelJinjin Chen0Xing Shen1Fanfan Tu2Ehtesham Mustafa Qureshi3State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaWind tunnels usually use long cantilever stings to support aerodynamic models in order to reduce support system flow interference on experimental data. However, such support systems are a potential source of vibration problems which limit the test envelope and affect data quality due to the inherently low structural damping of the systems. When exposed to tunnel flow, turbulence and model flow separation excite resonant Eigenmodes of a sting structure causing large vibrations due to low damping. This paper details the development and experimental evaluation of an active damping system using piezoelectric devices with balance signal feedback both in a lab and a low speed acoustic wind tunnel and presents the control algorithm verification tests with a simple cantilever beam. It is shown that the active damper, controlled separately by both PID and BP neural network, has effectively attenuated the vibration. For sting mode only, 95% reduction of displacement response under exciter stimulation and 98% energy elimination of sting mode frequency have been achieved.http://dx.doi.org/10.1155/2014/524351
collection DOAJ
language English
format Article
sources DOAJ
author Jinjin Chen
Xing Shen
Fanfan Tu
Ehtesham Mustafa Qureshi
spellingShingle Jinjin Chen
Xing Shen
Fanfan Tu
Ehtesham Mustafa Qureshi
Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
Shock and Vibration
author_facet Jinjin Chen
Xing Shen
Fanfan Tu
Ehtesham Mustafa Qureshi
author_sort Jinjin Chen
title Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
title_short Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
title_full Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
title_fullStr Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
title_full_unstemmed Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel
title_sort experimental research on an active sting damper in a low speed acoustic wind tunnel
publisher Hindawi Limited
series Shock and Vibration
issn 1070-9622
1875-9203
publishDate 2014-01-01
description Wind tunnels usually use long cantilever stings to support aerodynamic models in order to reduce support system flow interference on experimental data. However, such support systems are a potential source of vibration problems which limit the test envelope and affect data quality due to the inherently low structural damping of the systems. When exposed to tunnel flow, turbulence and model flow separation excite resonant Eigenmodes of a sting structure causing large vibrations due to low damping. This paper details the development and experimental evaluation of an active damping system using piezoelectric devices with balance signal feedback both in a lab and a low speed acoustic wind tunnel and presents the control algorithm verification tests with a simple cantilever beam. It is shown that the active damper, controlled separately by both PID and BP neural network, has effectively attenuated the vibration. For sting mode only, 95% reduction of displacement response under exciter stimulation and 98% energy elimination of sting mode frequency have been achieved.
url http://dx.doi.org/10.1155/2014/524351
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AT xingshen experimentalresearchonanactivestingdamperinalowspeedacousticwindtunnel
AT fanfantu experimentalresearchonanactivestingdamperinalowspeedacousticwindtunnel
AT ehteshammustafaqureshi experimentalresearchonanactivestingdamperinalowspeedacousticwindtunnel
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