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A '''circulation control wing''' (CCW) is a form of [[high-lift device]] for use on the main wing of an aircraft to increase the maximum [[lift coefficient]] and reduce the [[stalling speed]]. CCW technology has been in the research and development phase for over sixty years. [[Blown flaps]] were an early example of CCW.<ref name="Circulation Control Wing">{{cite web |url=http://www.sae.org/technical/papers/2005-01-3192 |title= A Propulsion Concept for Circulation Control Wing Technology |accessdate=2024-07-27 |archive-url=https://web.archive.org/web/20080102083136/http://www.sae.org/technical/papers/2005-01-3192 |archive-date=2008-01-02 |url-status=dead |publisher=[[SAE International]]}}</ref>
The CCW works by increasing the velocity of the airflow over the [[leading edge]] and [[trailing edge]] of a specially designed aircraft [[wing]] using a series of blowing slots that eject jets of high-pressure air. The wing has a rounded trailing edge to tangentially eject the air through the [[Coandă effect]] thus causing lift.<ref name="Slomski">{{cite
[[Image:Circulation Control Airfoil.svg|thumb|The [[trailing edge]] of a CCW showing the blowing slot and tangential [[coanda]] airflow.]]
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== Powering the wing ==
The main problem with the circulation control wing is the need for high energy air to be blown over the wing's surface. Such air is often [[Bleed air|bled from the engine]]; however, this drastically reduces engine power production and consequently counteracts the purpose of the wing. Other options are taking the exhaust gases (which must first be cooled) or using multiple, lightweight gas generators, which are separate from the main aircraft engines.<ref name="Circulation Control Wing"/>
==See also==
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