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- Circulation_control_wing abstract "A circulation control wing (CCW) is a form of high-lift device for use on the main wing of an aircraft to increase the lift coefficient. CCW technology has been in the research and development phase for over sixty years, and the early models were called blown flaps.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 high pressure jet air. The wing has a rounded trailing edge to tangentially eject the air through the Coandă effect thus causing lift. The increase in velocity of the airflow over the wing also adds to the lift force through conventional airfoil lift production.".
- Circulation_control_wing thumbnail Circulation_Control_Airfoil.svg?width=300.
- Circulation_control_wing wikiPageID "14713337".
- Circulation_control_wing wikiPageRevisionID "605078284".
- Circulation_control_wing hasPhotoCollection Circulation_control_wing.
- Circulation_control_wing subject Category:Aerodynamics.
- Circulation_control_wing subject Category:Aircraft_wing_components.
- Circulation_control_wing comment "A circulation control wing (CCW) is a form of high-lift device for use on the main wing of an aircraft to increase the lift coefficient. CCW technology has been in the research and development phase for over sixty years, and the early models were called blown flaps.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 high pressure jet air.".
- Circulation_control_wing label "Circulation control wing".
- Circulation_control_wing sameAs m.03gv0dw.
- Circulation_control_wing sameAs Q5121691.
- Circulation_control_wing sameAs Q5121691.
- Circulation_control_wing wasDerivedFrom Circulation_control_wing?oldid=605078284.
- Circulation_control_wing depiction Circulation_Control_Airfoil.svg.
- Circulation_control_wing isPrimaryTopicOf Circulation_control_wing.
