<?xml version="1.0" encoding="UTF-8"?>        <rss version="2.0"
             xmlns:atom="http://www.w3.org/2005/Atom"
             xmlns:dc="http://purl.org/dc/elements/1.1/"
             xmlns:sy="http://purl.org/rss/1.0/modules/syndication/"
             xmlns:admin="http://webns.net/mvcb/"
             xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#"
             xmlns:content="http://purl.org/rss/1.0/modules/content/">
        <channel>
            <title>
									&quot;A viscous flow moves over a flat plate of length L. As the flow continues, the boundary layer grows quickly. At the transition point, the boundary layer thickness is δ. What is the value of the velocity potential function ɸ for this flow?&quot; - Aerodynamics &amp; Flight Mechanics				            </title>
            <link>https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/a-viscous-flow-moves-over-a-flat-plate-of-length-l-as-the-flow-continues-the-boundary-layer-grows-quickly-at-the-transition-point-the-boundary-layer-thickness-is-%ce%b4-what-is-the-value-of-the/</link>
            <description>IITians Gate Academy Discussion Board</description>
            <language>en-US</language>
            <lastBuildDate>Mon, 16 Mar 2026 15:45:13 +0000</lastBuildDate>
            <generator>wpForo</generator>
            <ttl>60</ttl>
							                    <item>
                        <title>RE: &quot;A viscous flow moves over a flat plate of length L. As the flow continues, the boundary layer grows quickly. At the transition point, the boundary layer thickness is δ. What is the value of the velocity potential function ɸ for this flow?&quot;</title>
                        <link>https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/a-viscous-flow-moves-over-a-flat-plate-of-length-l-as-the-flow-continues-the-boundary-layer-grows-quickly-at-the-transition-point-the-boundary-layer-thickness-is-%ce%b4-what-is-the-value-of-the/#post-10</link>
                        <pubDate>Thu, 17 Jul 2025 16:11:52 +0000</pubDate>
                        <description><![CDATA[In viscous flow over a flat plate, a boundary layer forms and grows along the plate. Inside this layer, the flow has friction and rotation. Since the velocity potential only exists in fricti...]]></description>
                        <content:encoded><![CDATA[<p>In viscous flow over a flat plate, a boundary layer forms and grows along the plate. Inside this layer, the flow has friction and rotation. Since the <strong data-start="150" data-end="172">velocity potential</strong> only exists in frictionless, smooth (irrotational) flow, <strong data-start="230" data-end="249">it is not valid</strong> in this case.</p>
<p data-start="266" data-end="343" data-is-last-node="" data-is-only-node=""><strong data-start="266" data-end="343" data-is-last-node="">So, the velocity potential function does not exist for this viscous flow.</strong></p>]]></content:encoded>
						                            <category domain="https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/">Aerodynamics &amp; Flight Mechanics</category>                        <dc:creator>krishna Kumar</dc:creator>
                        <guid isPermaLink="true">https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/a-viscous-flow-moves-over-a-flat-plate-of-length-l-as-the-flow-continues-the-boundary-layer-grows-quickly-at-the-transition-point-the-boundary-layer-thickness-is-%ce%b4-what-is-the-value-of-the/#post-10</guid>
                    </item>
				                    <item>
                        <title>&quot;A viscous flow moves over a flat plate of length L. As the flow continues, the boundary layer grows quickly. At the transition point, the boundary layer thickness is δ. What is the value of the velocity potential function ɸ for this flow?&quot;</title>
                        <link>https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/a-viscous-flow-moves-over-a-flat-plate-of-length-l-as-the-flow-continues-the-boundary-layer-grows-quickly-at-the-transition-point-the-boundary-layer-thickness-is-%ce%b4-what-is-the-value-of-the/#post-9</link>
                        <pubDate>Thu, 17 Jul 2025 16:10:05 +0000</pubDate>
                        <description><![CDATA[&quot;A viscous flow moves over a flat plate of length L. As the flow continues, the boundary layer grows quickly. At the transition point, the boundary layer thickness is δ. What is the value of...]]></description>
                        <content:encoded><![CDATA[<p>"A viscous flow moves over a flat plate of length L. As the flow continues, the boundary layer grows quickly. At the transition point, the boundary layer thickness is δ. What is the value of the velocity potential function ɸ for this flow?"</p>]]></content:encoded>
						                            <category domain="https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/">Aerodynamics &amp; Flight Mechanics</category>                        <dc:creator>krishna Kumar</dc:creator>
                        <guid isPermaLink="true">https://iitiansgateacademy.com/community/aerodynamics-flight-mechanics/a-viscous-flow-moves-over-a-flat-plate-of-length-l-as-the-flow-continues-the-boundary-layer-grows-quickly-at-the-transition-point-the-boundary-layer-thickness-is-%ce%b4-what-is-the-value-of-the/#post-9</guid>
                    </item>
							        </channel>
        </rss>
		