<?xml version="1.0" encoding="utf-8" standalone="yes"?>
<rss version="2.0" xmlns:atom="http://www.w3.org/2005/Atom">
  <channel>
    <title>Falkner-Skan on An album of computational fluid motion</title>
    <link>https://album-of-cfm.com/tags/falkner-skan/</link>
    <description>Recent content in Falkner-Skan on An album of computational fluid motion</description>
    <generator>Hugo -- gohugo.io</generator>
    <language>en</language>
    <lastBuildDate>Mon, 28 Jul 2025 00:00:00 +0000</lastBuildDate><atom:link href="https://album-of-cfm.com/tags/falkner-skan/index.xml" rel="self" type="application/rss+xml" />
    <item>
      <title>Fig 23. Symmetric plane flow past an airfoil</title>
      <link>https://album-of-cfm.com/chapters/02-laminar/fig23/</link>
      <pubDate>Mon, 28 Jul 2025 00:00:00 +0000</pubDate>
      
      <guid>https://album-of-cfm.com/chapters/02-laminar/fig23/</guid>
      <description>ExperimentSimulation &amp;ldquo;An NACA 64A015 profile is at zero incidence in a water tunnel. The Reynolds number is 7000 based on the chordlength. Streamlines are shown by colored fluid introduced upstream.</description>
    </item>
    
  </channel>
</rss>
