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	<title>Boeing 737 MAX 8 &#8211; BIOENGINEER.ORG</title>
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		<title>Simulated 737 MAX 8 reveals transonic shocks and peak cruise efficiency</title>
		<link>https://bioengineer.org/simulated-737-max-8-reveals-transonic-shocks-and-peak-cruise-efficiency/</link>
		
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		<pubDate>Mon, 26 Oct 2026 17:51:28 +0000</pubDate>
				<category><![CDATA[Technology]]></category>
		<category><![CDATA[aerodynamic]]></category>
		<category><![CDATA[aerodynamics]]></category>
		<category><![CDATA[aerospace systems]]></category>
		<category><![CDATA[Boeing]]></category>
		<category><![CDATA[Boeing 737 MAX 8]]></category>
		<category><![CDATA[Computational fluid dynamics]]></category>
		<category><![CDATA[critical Mach number]]></category>
		<category><![CDATA[drag divergence]]></category>
		<category><![CDATA[shock boundary layer interaction]]></category>
		<category><![CDATA[Spalart-Allmaras]]></category>
		<category><![CDATA[transonic flow]]></category>
		<category><![CDATA[wingtip vortices]]></category>
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					<description><![CDATA[A computational study of a simplified Boeing 737 MAX 8 in cruise condition identified a representative baseline configuration, a critical Mach number of 0.6108, and maximum aerodynamic efficiency at roughly 2 degrees angle of attack.]]></description>
		
		
		
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