Calibration of strain gage instrumentation for an aircraft pylon

This final year project developed a load calibration strain gage procedure and system for a F16 non-jettisonable fuel pylon with an existing fixture. The system identified the best strain gage bridge for load calibration. Most importantly, the substitutes for the best strain gage bridges were identi...

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Main Author: Tan, Alan Dao Yang
Other Authors: Sunil Chandrakant Joshi
Format: Final Year Project
Language:English
Published: 2011
Subjects:
Online Access:http://hdl.handle.net/10356/45249
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-452492023-03-04T18:26:16Z Calibration of strain gage instrumentation for an aircraft pylon Tan, Alan Dao Yang Sunil Chandrakant Joshi School of Mechanical and Aerospace Engineering Republic of Singapore Air Force DRNTU::Engineering::Aeronautical engineering::Instruments This final year project developed a load calibration strain gage procedure and system for a F16 non-jettisonable fuel pylon with an existing fixture. The system identified the best strain gage bridge for load calibration. Most importantly, the substitutes for the best strain gage bridges were identified, which becomes a solution for a damaged strain gage bridge as the next best strain gage bridge that can be used for load calibration. In order to develop the system, a study was done on the least square regression method and the equations that are derived for the method. The method for derivation of the load equation is tedious. Therefore an automated system was created to analyze the characteristic of the load equations of different stain gage bridges combination. In addition, an interface that is user friendly was designed to allow individuals with no computing knowledge to enjoy the benefits of the computing program. Bachelor of Engineering (Aerospace Engineering) 2011-06-10T04:29:06Z 2011-06-10T04:29:06Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/45249 en Nanyang Technological University 154 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Instruments
spellingShingle DRNTU::Engineering::Aeronautical engineering::Instruments
Tan, Alan Dao Yang
Calibration of strain gage instrumentation for an aircraft pylon
description This final year project developed a load calibration strain gage procedure and system for a F16 non-jettisonable fuel pylon with an existing fixture. The system identified the best strain gage bridge for load calibration. Most importantly, the substitutes for the best strain gage bridges were identified, which becomes a solution for a damaged strain gage bridge as the next best strain gage bridge that can be used for load calibration. In order to develop the system, a study was done on the least square regression method and the equations that are derived for the method. The method for derivation of the load equation is tedious. Therefore an automated system was created to analyze the characteristic of the load equations of different stain gage bridges combination. In addition, an interface that is user friendly was designed to allow individuals with no computing knowledge to enjoy the benefits of the computing program.
author2 Sunil Chandrakant Joshi
author_facet Sunil Chandrakant Joshi
Tan, Alan Dao Yang
format Final Year Project
author Tan, Alan Dao Yang
author_sort Tan, Alan Dao Yang
title Calibration of strain gage instrumentation for an aircraft pylon
title_short Calibration of strain gage instrumentation for an aircraft pylon
title_full Calibration of strain gage instrumentation for an aircraft pylon
title_fullStr Calibration of strain gage instrumentation for an aircraft pylon
title_full_unstemmed Calibration of strain gage instrumentation for an aircraft pylon
title_sort calibration of strain gage instrumentation for an aircraft pylon
publishDate 2011
url http://hdl.handle.net/10356/45249
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