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    <title>Boundary layer on An album of computational fluid motion</title>
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    <description>Recent content in Boundary layer on An album of computational fluid motion</description>
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      <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>
      
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      <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>
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    <item>
      <title>Fig 34. Boundary-layer separation on an inclined airfoil</title>
      <link>https://album-of-cfm.com/chapters/03-separation/fig34/</link>
      <pubDate>Mon, 28 Jul 2025 00:00:00 +0000</pubDate>
      
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      <description>ExperimentSimulation &amp;ldquo;When the NACA 64A015 airfoil of figure 23 is raised to 5\(\degree\) incidence the laminar boundary layer separates from the rear half of the upper surface. The flow remains attached to the lower surface, from which it leaves tangentially at the trailing edge.</description>
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