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In ''Aerodynamics'' a '''stall''' is a condition in which an excessive [[angle of attack]] causes a separation of airflow on the upper surface of the wing. The stall is manifested by a corresponding increase in drag and a rapid loss of lift.
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http://en.wikipedia.org/wiki/Stall
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More information at Wikipedia: [http://en.wikipedia.org/wiki/Stall]
 
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[[Category: Articles]]
 
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[[Category:Glossary]]
 
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[[Category:Aerodynamics]]
 
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{{Stub}}
 

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