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	<title>Zero-Lift Drag - Revision history</title>
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	<updated>2026-07-20T18:30:20Z</updated>
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		<id>https://wiki.alsresume.com/index.php?title=Zero-Lift_Drag&amp;diff=29644&amp;oldid=prev</id>
		<title>wikipedia&gt;Unknown user at 20:55, 26 April 2025</title>
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		<updated>2025-04-26T20:55:00Z</updated>

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		<author><name>wikipedia&gt;Unknown user</name></author>
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		<id>https://wiki.alsresume.com/index.php?title=Zero-Lift_Drag&amp;diff=29645&amp;oldid=prev</id>
		<title>Admin: 1 revision imported</title>
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		<updated>2025-04-26T20:27:31Z</updated>

		<summary type="html">&lt;p&gt;1 revision imported&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;&amp;#039;&amp;#039;&amp;#039;Zero-Lift Drag&amp;#039;&amp;#039;&amp;#039; refers to the aerodynamic resistance encountered by an aircraft when it is producing no lift.&lt;br /&gt;
&lt;br /&gt;
== Definition ==&lt;br /&gt;
Zero-lift drag, also known as parasite drag, is the sum of all aerodynamic forces opposing an aircraft&amp;#039;s motion through the air when no lift is being generated. It includes form drag, skin friction drag, and interference drag.&lt;br /&gt;
&lt;br /&gt;
== Components ==&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Form Drag&amp;#039;&amp;#039;&amp;#039;: Caused by the shape and frontal area of the aircraft disrupting airflow.&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Skin Friction Drag&amp;#039;&amp;#039;&amp;#039;: Generated by air moving across the surface of the aircraft.&lt;br /&gt;
* &amp;#039;&amp;#039;&amp;#039;Interference Drag&amp;#039;&amp;#039;&amp;#039;: Results from the interaction of airflow at junctions like wing-fuselage connections.&lt;br /&gt;
&lt;br /&gt;
== Importance ==&lt;br /&gt;
* Minimizing zero-lift drag is critical to improving fuel efficiency and performance.&lt;br /&gt;
* Engineers use streamlined designs, smooth surfaces, and aerodynamic fairings to reduce these drag components.&lt;br /&gt;
* Impacts cruise speed, range, and climb performance of the aircraft.&lt;br /&gt;
&lt;br /&gt;
== Measurement ==&lt;br /&gt;
Zero-lift drag is often quantified by the drag coefficient \( C_{D0} \), representing the baseline drag of the aircraft without any lift contribution.&lt;br /&gt;
&lt;br /&gt;
== Practical Applications ==&lt;br /&gt;
* Designing more efficient airframes and aerodynamic profiles.&lt;br /&gt;
* Establishing baseline performance models for aircraft during certification and testing.&lt;br /&gt;
* Informing computational fluid dynamics (CFD) studies and wind tunnel experiments.&lt;br /&gt;
&lt;br /&gt;
== Example ==&lt;br /&gt;
During straight and level cruise flight, engineers aim to reduce the aircraft&amp;#039;s zero-lift drag to optimize range and fuel consumption, often by refining the fuselage shape and minimizing protrusions.&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
* [https://en.wikipedia.org/wiki/Parasitic_drag Parasitic Drag - Wikipedia]&lt;br /&gt;
* [https://www.grc.nasa.gov/www/k-12/airplane/drag.html NASA - Drag Sources and Reduction Techniques]&lt;br /&gt;
* [https://www.skybrary.aero/articles/drag-sources Drag Sources - SKYbrary]&lt;br /&gt;
* [https://ntrs.nasa.gov/citations/19980228112 NASA - Drag Analysis Techniques]&lt;br /&gt;
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		<author><name>Admin</name></author>
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