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- Parker_Variable_Wing abstract "The Parker Variable Wing is a wing configuration in biplane or triplane aircraft designed by H.F. Parker in 1920. His design allows a supplement in lift while landing or taking-off.The system is depicted in the figure. The figure shows the biplane configuration. The lower airfoil is rigid. The upper airfoil is flexible. At high angle of attack the flow over the lower airfoil will cause the airflow to bend up and create an upward force at the lower surface of the upper airfoil. This upward force will cause the flexible section to bepushed upward. The flexible wing section is held at points A and B. The trailing edge is rigid and can rotate about point B. Due to this effect the camber of the airfoil is increased, and hence the lift it creates is increased.".
- Parker_Variable_Wing thumbnail Smooth_camber.jpg?width=300.
- Parker_Variable_Wing wikiPageID "6454634".
- Parker_Variable_Wing wikiPageLength "1200".
- Parker_Variable_Wing wikiPageOutDegree "14".
- Parker_Variable_Wing wikiPageRevisionID "517391531".
- Parker_Variable_Wing wikiPageWikiLink Adaptive_Compliant_Wing.
- Parker_Variable_Wing wikiPageWikiLink Adaptive_compliant_wing.
- Parker_Variable_Wing wikiPageWikiLink Aeroelasticity.
- Parker_Variable_Wing wikiPageWikiLink Airfoil.
- Parker_Variable_Wing wikiPageWikiLink Angle_of_attack.
- Parker_Variable_Wing wikiPageWikiLink Biplane.
- Parker_Variable_Wing wikiPageWikiLink Boeing_X-53_Active_Aeroelastic_Wing.
- Parker_Variable_Wing wikiPageWikiLink Camber_(aerodynamics).
- Parker_Variable_Wing wikiPageWikiLink Category:Aerodynamics.
- Parker_Variable_Wing wikiPageWikiLink Category:Aerospace_engineering.
- Parker_Variable_Wing wikiPageWikiLink Category:Aircraft_wing_design.
- Parker_Variable_Wing wikiPageWikiLink H.F._Parker.
- Parker_Variable_Wing wikiPageWikiLink Trailing_edge.
- Parker_Variable_Wing wikiPageWikiLink Triplane.
- Parker_Variable_Wing wikiPageWikiLink X-53_Active_Aeroelastic_Wing.
- Parker_Variable_Wing wikiPageWikiLink File:Smooth_camber.jpg.
- Parker_Variable_Wing wikiPageWikiLinkText "Parker Variable Wing".
- Parker_Variable_Wing hasPhotoCollection Parker_Variable_Wing.
- Parker_Variable_Wing wikiPageUsesTemplate Template:One_source.
- Parker_Variable_Wing subject Category:Aerodynamics.
- Parker_Variable_Wing subject Category:Aerospace_engineering.
- Parker_Variable_Wing subject Category:Aircraft_wing_design.
- Parker_Variable_Wing hypernym Configuration.
- Parker_Variable_Wing type Aircraft.
- Parker_Variable_Wing type Article.
- Parker_Variable_Wing type Aeronautic.
- Parker_Variable_Wing type Article.
- Parker_Variable_Wing type Component.
- Parker_Variable_Wing type Discipline.
- Parker_Variable_Wing type Dynamic.
- Parker_Variable_Wing type Technology.
- Parker_Variable_Wing comment "The Parker Variable Wing is a wing configuration in biplane or triplane aircraft designed by H.F. Parker in 1920. His design allows a supplement in lift while landing or taking-off.The system is depicted in the figure. The figure shows the biplane configuration. The lower airfoil is rigid. The upper airfoil is flexible. At high angle of attack the flow over the lower airfoil will cause the airflow to bend up and create an upward force at the lower surface of the upper airfoil.".
- Parker_Variable_Wing label "Parker Variable Wing".
- Parker_Variable_Wing sameAs m.0g5zv1.
- Parker_Variable_Wing sameAs Q7138391.
- Parker_Variable_Wing sameAs Q7138391.
- Parker_Variable_Wing wasDerivedFrom Parker_Variable_Wing?oldid=517391531.
- Parker_Variable_Wing depiction Smooth_camber.jpg.
- Parker_Variable_Wing isPrimaryTopicOf Parker_Variable_Wing.