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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. | 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. | ||
More information at Wikipedia: [http://en.wikipedia.org/wiki/Stall] | More information at Wikipedia: [http://en.wikipedia.org/wiki/Stall] | ||
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[[Category:Glossary]] | [[Category:Glossary]] | ||
[[Category:Aerodynamics]] | [[Category:Aerodynamics]] | ||
{{Stub}} | {{Stub}} |