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	<id>https:///index.php?action=history&amp;feed=atom&amp;title=Textile_composite_heat_transfer</id>
	<title>Textile composite heat transfer - Revision history</title>
	<link rel="self" type="application/atom+xml" href="https:///index.php?action=history&amp;feed=atom&amp;title=Textile_composite_heat_transfer"/>
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	<updated>2026-08-14T11:11:11Z</updated>
	<subtitle>Revision history for this page on the wiki</subtitle>
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	<entry>
		<id></id>
		<title>Joncrookston at 17:56, 13 March 2007</title>
		<link rel="alternate" type="text/html" href=""/>
		<updated>2007-03-13T17:56:32Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table class=&quot;diff diff-contentalign-left diff-editfont-monospace&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 17:56, 13 March 2007&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l6&quot; &gt;Line 6:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 6:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt;−&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;are &lt;/del&gt;through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &amp;quot;Prediction of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement geometry&amp;quot;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &amp;quot;Parametric unit cell modelling of the effective transverse thermal conductivity of carbon plain weave composites&amp;quot;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were seen within cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall volume fraction could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;or &lt;/ins&gt;through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &amp;quot;Prediction of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement geometry&amp;quot;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &amp;quot;Parametric unit cell modelling of the effective transverse thermal conductivity of carbon plain weave composites&amp;quot;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were seen within cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall volume fraction could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Joncrookston</name></author>
	</entry>
	<entry>
		<id></id>
		<title>WikiSysop at 17:39, 13 March 2007</title>
		<link rel="alternate" type="text/html" href=""/>
		<updated>2007-03-13T17:39:58Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table class=&quot;diff diff-contentalign-left diff-editfont-monospace&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 17:39, 13 March 2007&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l6&quot; &gt;Line 6:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 6:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt;−&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models are through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &amp;quot;Prediction of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement geometry&amp;quot;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &amp;quot;Parametric unit cell modelling of the effective transverse thermal conductivity of carbon plain weave composites&amp;quot;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;seem with in &lt;/del&gt;cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;vf &lt;/del&gt;could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models are through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &amp;quot;Prediction of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement geometry&amp;quot;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &amp;quot;Parametric unit cell modelling of the effective transverse thermal conductivity of carbon plain weave composites&amp;quot;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;seen within &lt;/ins&gt;cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;volume fraction &lt;/ins&gt;could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>WikiSysop</name></author>
	</entry>
	<entry>
		<id></id>
		<title>WikiSysop at 17:33, 13 March 2007</title>
		<link rel="alternate" type="text/html" href=""/>
		<updated>2007-03-13T17:33:42Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table class=&quot;diff diff-contentalign-left diff-editfont-monospace&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 17:33, 13 March 2007&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1&quot; &gt;Line 1:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;TexGen has been used to model steady-state thermal conduction in textile composites.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;TexGen has been used to model steady-state thermal conduction in textile composites.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;[[Image:Heatflux.png|thumb|Transverse heat flux in a non-crimp, carbon-reinforced composite]]&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;[[Image:Thermalcond.png|thumb|Natural variation of the thermal conductivity resulting from geometric changes, superimposed to the linear trend – results obtained from simulations]]&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>WikiSysop</name></author>
	</entry>
	<entry>
		<id></id>
		<title>WikiSysop at 17:26, 13 March 2007</title>
		<link rel="alternate" type="text/html" href=""/>
		<updated>2007-03-13T17:26:28Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table class=&quot;diff diff-contentalign-left diff-editfont-monospace&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 17:26, 13 March 2007&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l3&quot; &gt;Line 3:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 3:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt;−&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models are through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;“Prediction &lt;/del&gt;of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;geometry”&lt;/del&gt;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;“Parametric &lt;/del&gt;unit cell modelling of the effective transverse thermal conductivity of carbon plain weave &lt;del class=&quot;diffchange diffchange-inline&quot;&gt;composites”&lt;/del&gt;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were seem with in cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall vf could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models are through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;&amp;quot;Prediction &lt;/ins&gt;of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;geometry&amp;quot;&lt;/ins&gt;, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;&amp;quot;Parametric &lt;/ins&gt;unit cell modelling of the effective transverse thermal conductivity of carbon plain weave &lt;ins class=&quot;diffchange diffchange-inline&quot;&gt;composites&amp;quot;&lt;/ins&gt;, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were seem with in cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall vf could be quantified.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt; &lt;/td&gt;&lt;td style=&quot;background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;==References==&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot;&gt; &lt;/td&gt;&lt;td class=&#039;diff-marker&#039;&gt;+&lt;/td&gt;&lt;td style=&quot;color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;&amp;lt;references/&amp;gt;&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>WikiSysop</name></author>
	</entry>
	<entry>
		<id></id>
		<title>WikiSysop at 17:25, 13 March 2007</title>
		<link rel="alternate" type="text/html" href=""/>
		<updated>2007-03-13T17:25:31Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;TexGen has been used to model steady-state thermal conduction in textile composites. &lt;br /&gt;
&lt;br /&gt;
The objectives of the work are to predict the effect of the finer preform geometry on heat transfer and to offer a quantitative demonstration of the natural variability of physical properties in textile composites. In this case the physical phenomenon that is modelled is simple and the associated mathematical apparatus is well resolved. This allows stronger emphasis on the geometry of the preform and its effects.&lt;br /&gt;
&lt;br /&gt;
Beyond the different textile architectures the exact configuration taken by individual yarns within the dry textiles was prescribed, as opposed to being determined from mechanistic models are through appropriate observation techniques. Precise yarn sections and paths were varied systematically for non-crimp fabrics &amp;lt;ref&amp;gt;S. Hind, D. Raizenne, F. Robitaille. “Prediction of the effective transverse thermal conductivity of carbon based textile composites with varying constituent properties and reinforcement geometry”, Proc. Canada Japan Worshop on Composites, Toronto, Canada, 2006.&amp;lt;/ref&amp;gt; and weaves &amp;lt;ref&amp;gt;S. Hind, F. Robitaille, D. Raizenne. “Parametric unit cell modelling of the effective transverse thermal conductivity of carbon plain weave composites”, Proc. International Conference on Textile Composites (TEXCOMP-8), Nottingham, UK, 2006.&amp;lt;/ref&amp;gt;. Simulation results show the way in which parameters such as the yarn cross section aspect ratio, section shape, yarn thickness, yarn spacing and others affect the thermal conductivity. Furthermore, changes in conductivity were seem with in cases of varying yarn fibre volume fraction, where the overall fibre volume fractions was kept constant. As such, the variability in conductivity at constant overall vf could be quantified. &lt;br /&gt;
&lt;br /&gt;
Applications for the work range from carbon composite tooling for aerospace application and NRC/IAR (Ottawa) proprietary Smart Tooling technology, to thermal shielding and aircraft structural repair. Validation is ongoing for coupons using Hukseflux Thasys &amp;amp; Thisys apparatus, and for aircraft structures.&lt;/div&gt;</summary>
		<author><name>WikiSysop</name></author>
	</entry>
</feed>