Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels

The application of sandwich panel as insulating medium in aerospace industries is increasing in recent years as high strength to weight ratio of the structure is mandatory. Many researches were performed on customized honeycomb core sandwich panels to examine its thermal and acoustic insulating beha...

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Main Author: Antonyraj Zion Raj
Other Authors: Sunil Chandrakant Joshi
Format: Theses and Dissertations
Language:English
Published: 2016
Subjects:
Online Access:http://hdl.handle.net/10356/68591
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-685912023-03-11T17:13:41Z Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels Antonyraj Zion Raj Sunil Chandrakant Joshi School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering The application of sandwich panel as insulating medium in aerospace industries is increasing in recent years as high strength to weight ratio of the structure is mandatory. Many researches were performed on customized honeycomb core sandwich panels to examine its thermal and acoustic insulating behavior and the same was improved by filling the empty core cells with low thermal conducting material, such as, aerogel granules. This research reports on fabrication, quality assessment and thermal study on aerogel filled Glass Fiber Reinforced Bismalemide customized honeycomb core sandwich panel. A method to fabricate curved honeycomb core sandwich panel is discussed in this project. For assessing the bond quality at the core fill-face sheet interface, an active thermography technique is implemented. The bond quality between core fill and face sheet is characterized by the percentage rate of surface temperature dissipation at the bond area. The thermography technique adopts the principle of Pulsed Video Thermography method except the surface temperature dissipation rate is calculated using thermal images at known intervals of time instead of recording the thermal video. Thermal study on curved honeycomb sandwich panel is conducted to investigate its overall thermal insulation behavior. The thermal insulation capability of aerogel filled composite panel is exemplified by measuring the percentage of temperature loss through the thickness of the panel. A similar heat transfer study is performed on aerogel filled flat composite sandwich panels with different core thicknesses to scrutinize the effect of thickness on thermal insulation characteristics. The heat transfer study on aerogel filled BMI-GFRP sandwich panels evolved to a conclusion that the panel could insulate an average of 65% of temperature from thermally exposed surface to the other. Master of Science (Aerospace Engineering) 2016-05-27T07:32:57Z 2016-05-27T07:32:57Z 2016 Thesis http://hdl.handle.net/10356/68591 en 194 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
spellingShingle DRNTU::Engineering::Aeronautical engineering
Antonyraj Zion Raj
Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
description The application of sandwich panel as insulating medium in aerospace industries is increasing in recent years as high strength to weight ratio of the structure is mandatory. Many researches were performed on customized honeycomb core sandwich panels to examine its thermal and acoustic insulating behavior and the same was improved by filling the empty core cells with low thermal conducting material, such as, aerogel granules. This research reports on fabrication, quality assessment and thermal study on aerogel filled Glass Fiber Reinforced Bismalemide customized honeycomb core sandwich panel. A method to fabricate curved honeycomb core sandwich panel is discussed in this project. For assessing the bond quality at the core fill-face sheet interface, an active thermography technique is implemented. The bond quality between core fill and face sheet is characterized by the percentage rate of surface temperature dissipation at the bond area. The thermography technique adopts the principle of Pulsed Video Thermography method except the surface temperature dissipation rate is calculated using thermal images at known intervals of time instead of recording the thermal video. Thermal study on curved honeycomb sandwich panel is conducted to investigate its overall thermal insulation behavior. The thermal insulation capability of aerogel filled composite panel is exemplified by measuring the percentage of temperature loss through the thickness of the panel. A similar heat transfer study is performed on aerogel filled flat composite sandwich panels with different core thicknesses to scrutinize the effect of thickness on thermal insulation characteristics. The heat transfer study on aerogel filled BMI-GFRP sandwich panels evolved to a conclusion that the panel could insulate an average of 65% of temperature from thermally exposed surface to the other.
author2 Sunil Chandrakant Joshi
author_facet Sunil Chandrakant Joshi
Antonyraj Zion Raj
format Theses and Dissertations
author Antonyraj Zion Raj
author_sort Antonyraj Zion Raj
title Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
title_short Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
title_full Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
title_fullStr Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
title_full_unstemmed Thermal studies and bond quality assessment of aerogel filled BMI composite curved sandwich panels
title_sort thermal studies and bond quality assessment of aerogel filled bmi composite curved sandwich panels
publishDate 2016
url http://hdl.handle.net/10356/68591
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