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- Kutta_condition abstract "The Kutta condition is a principle in steady flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies which have sharp corners such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist Martin Wilhelm Kutta.Kuethe and Schetzer state the Kutta condition as follows:A body with a sharp trailing edge which is moving through a fluid will create about itself a circulation of sufficient strength to hold the rear stagnation point at the trailing edge.In fluid flow around a body with a sharp corner the Kutta condition refers to the flow pattern in which fluid approaches the corner from both directions, meets at the corner and then flows away from the body. None of the fluid flows around the corner and remains attached to the body.The Kutta condition is significant when using the Kutta–Joukowski theorem to calculate the lift created by an airfoil with generally cusped trailing edge. The value of circulation of the flow around the airfoil must be that value which would cause the Kutta condition to exist.".
- Kutta_condition wikiPageExternalLink node21.html.
- Kutta_condition wikiPageExternalLink profilo_e.html.
- Kutta_condition wikiPageID "4265190".
- Kutta_condition wikiPageLength "10116".
- Kutta_condition wikiPageOutDegree "40".
- Kutta_condition wikiPageRevisionID "675650695".
- Kutta_condition wikiPageWikiLink Aerodynamics.
- Kutta_condition wikiPageWikiLink Airfoil.
- Kutta_condition wikiPageWikiLink Angle_of_attack.
- Kutta_condition wikiPageWikiLink Boundary_layer.
- Kutta_condition wikiPageWikiLink Category:Aerodynamics.
- Kutta_condition wikiPageWikiLink Category:Fluid_dynamics.
- Kutta_condition wikiPageWikiLink Circulation_(fluid_dynamics).
- Kutta_condition wikiPageWikiLink Conservation_of_mass.
- Kutta_condition wikiPageWikiLink Conservation_of_momentum.
- Kutta_condition wikiPageWikiLink Fluid_dynamics.
- Kutta_condition wikiPageWikiLink Germany.
- Kutta_condition wikiPageWikiLink Horseshoe_vortex.
- Kutta_condition wikiPageWikiLink Kelvins_circulation_theorem.
- Kutta_condition wikiPageWikiLink Kutta–Joukowski_theorem.
- Kutta_condition wikiPageWikiLink Lift_(force).
- Kutta_condition wikiPageWikiLink Martin_Wilhelm_Kutta.
- Kutta_condition wikiPageWikiLink Mathematician.
- Kutta_condition wikiPageWikiLink Momentum.
- Kutta_condition wikiPageWikiLink Navier–Stokes_equations.
- Kutta_condition wikiPageWikiLink Parasitic_drag.
- Kutta_condition wikiPageWikiLink Potential_flow.
- Kutta_condition wikiPageWikiLink Skin_friction.
- Kutta_condition wikiPageWikiLink Stagnation_point.
- Kutta_condition wikiPageWikiLink Starting_vortex.
- Kutta_condition wikiPageWikiLink Trailing_edge.
- Kutta_condition wikiPageWikiLink Viscosity.
- Kutta_condition wikiPageWikiLink Vortex.
- Kutta_condition wikiPageWikiLink Vorticity.
- Kutta_condition wikiPageWikiLink Wing.
- Kutta_condition wikiPageWikiLinkText "Kutta condition".
- Kutta_condition hasPhotoCollection Kutta_condition.
- Kutta_condition wikiPageUsesTemplate Template:Reflist.
- Kutta_condition subject Category:Aerodynamics.
- Kutta_condition subject Category:Fluid_dynamics.
- Kutta_condition hypernym Principle.
- Kutta_condition type Airline.
- Kutta_condition type Dynamic.
- Kutta_condition type Mechanic.
- Kutta_condition comment "The Kutta condition is a principle in steady flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies which have sharp corners such as the trailing edges of airfoils.".
- Kutta_condition label "Kutta condition".
- Kutta_condition sameAs Condizione_di_Kutta.
- Kutta_condition sameAs Condição_de_Kutta.
- Kutta_condition sameAs m.0bt376.
- Kutta_condition sameAs Постулат_Жуковского_—_Чаплыгина.
- Kutta_condition sameAs Q1154278.
- Kutta_condition sameAs Q1154278.
- Kutta_condition wasDerivedFrom Kutta_condition?oldid=675650695.
- Kutta_condition isPrimaryTopicOf Kutta_condition.