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- Kutta–Joukowski_theorem abstract "The Kutta–Joukowski theorem is a fundamental theorem of aerodynamics, that can be used for the calculation of the lift of an airfoil, or of any two-dimensional bodies including circular cylinders, translating in a uniform fluid at a constant speed large enough so that the flow seen in the body-fixed frame is steady and unseparated. The theorem relates the lift generated by an airfoil to the speed of the airfoil through the fluid, the density of the fluid, and the circulation. The circulation is defined as the line integral, around a closed loop enclosing the airfoil, of the component of the velocity of the fluid tangent to the loop. It is named after the German Martin Wilhelm Kutta and the Russian Nikolai Zhukovsky (or Joukowski) who first developed its key ideas in the early 20th century. Kutta–Joukowski theorem is an inviscid theory which for pressure and lift is however a good approximation to real viscous flow for typical aerodynamic applications. Kutta–Joukowski theorem relates lift to circulation much like the Magnus effect relates side force (called Magnus force) to rotation. However, circulation here is not induced by rotation of the airfoil but by some intrinsic mechanism described below. Due to this circulation, the flow of air in response to the presence of the airfoil can be treated as the superposition of a translational flow and a rotating flow. This rotating flow is induced by joint effect of camber, angle of attack and sharp trailing edge of the airfoil and should not be confused with a vortex like a tornado encircling the cylinder or the wing of an airplane in flight. Seen from a distance large enough to the airfoil, this rotating flow may be regarded as induced by a line vortex (with the rotating line perpendicular to the twodimensional plane). In the derivation of the Kutta–Joukowski theorem the airfoil is usually mapped into a circular cylinder. This theorem is proved in many text books only for circular cylinder and Joukowski airfoil, but it holds true for general airfoils.".
- Kutta–Joukowski_theorem wikiPageID "8606325".
- Kutta–Joukowski_theorem wikiPageLength "21932".
- Kutta–Joukowski_theorem wikiPageOutDegree "47".
- Kutta–Joukowski_theorem wikiPageRevisionID "694963313".
- Kutta–Joukowski_theorem wikiPageWikiLink Aerodynamics.
- Kutta–Joukowski_theorem wikiPageWikiLink Airfoil.
- Kutta–Joukowski_theorem wikiPageWikiLink Bernoullis_principle.
- Kutta–Joukowski_theorem wikiPageWikiLink Blasius–Chaplygin_formula.
- Kutta–Joukowski_theorem wikiPageWikiLink Boundary_layer.
- Kutta–Joukowski_theorem wikiPageWikiLink Category:Aerodynamics.
- Kutta–Joukowski_theorem wikiPageWikiLink Category:Fluid_dynamics.
- Kutta–Joukowski_theorem wikiPageWikiLink Category:Physics_theorems.
- Kutta–Joukowski_theorem wikiPageWikiLink Chord_(aeronautics).
- Kutta–Joukowski_theorem wikiPageWikiLink Circulation_(fluid_dynamics).
- Kutta–Joukowski_theorem wikiPageWikiLink Complex_analysis.
- Kutta–Joukowski_theorem wikiPageWikiLink Complex_conjugate.
- Kutta–Joukowski_theorem wikiPageWikiLink Complex_number.
- Kutta–Joukowski_theorem wikiPageWikiLink Complex_plane.
- Kutta–Joukowski_theorem wikiPageWikiLink Complex_potential.
- Kutta–Joukowski_theorem wikiPageWikiLink Differential_(mathematics).
- Kutta–Joukowski_theorem wikiPageWikiLink George_Batchelor.
- Kutta–Joukowski_theorem wikiPageWikiLink Germany.
- Kutta–Joukowski_theorem wikiPageWikiLink Heuristic.
- Kutta–Joukowski_theorem wikiPageWikiLink Holomorphic_function.
- Kutta–Joukowski_theorem wikiPageWikiLink Horseshoe_vortex.
- Kutta–Joukowski_theorem wikiPageWikiLink Inviscid_flow.
- Kutta–Joukowski_theorem wikiPageWikiLink Joukowsky_transform.
- Kutta–Joukowski_theorem wikiPageWikiLink Kutta_condition.
- Kutta–Joukowski_theorem wikiPageWikiLink Laurent_series.
- Kutta–Joukowski_theorem wikiPageWikiLink Lift_(force).
- Kutta–Joukowski_theorem wikiPageWikiLink Lift_coefficient.
- Kutta–Joukowski_theorem wikiPageWikiLink Line_integral.
- Kutta–Joukowski_theorem wikiPageWikiLink Magnus_effect.
- Kutta–Joukowski_theorem wikiPageWikiLink Martin_Wilhelm_Kutta.
- Kutta–Joukowski_theorem wikiPageWikiLink Nikolay_Yegorovich_Zhukovsky.
- Kutta–Joukowski_theorem wikiPageWikiLink Potential_flow.
- Kutta–Joukowski_theorem wikiPageWikiLink Residue_theorem.
- Kutta–Joukowski_theorem wikiPageWikiLink Russians.
- Kutta–Joukowski_theorem wikiPageWikiLink Static_pressure.
- Kutta–Joukowski_theorem wikiPageWikiLink Stream_function.
- Kutta–Joukowski_theorem wikiPageWikiLink Superposition_principle.
- Kutta–Joukowski_theorem wikiPageWikiLink Tangent.
- Kutta–Joukowski_theorem wikiPageWikiLink Tornado.
- Kutta–Joukowski_theorem wikiPageWikiLink Unit_vector.
- Kutta–Joukowski_theorem wikiPageWikiLink Vector_calculus.
- Kutta–Joukowski_theorem wikiPageWikiLink Wing.
- Kutta–Joukowski_theorem wikiPageWikiLink Wingspan.
- Kutta–Joukowski_theorem wikiPageWikiLinkText "Kutta-Joukowski theorem".
- Kutta–Joukowski_theorem wikiPageWikiLinkText "Kutta–Joukowski theorem".
- Kutta–Joukowski_theorem wikiPageWikiLinkText "Kutta–Joukowski".
- Kutta–Joukowski_theorem wikiPageUsesTemplate Template:EquationNote.
- Kutta–Joukowski_theorem wikiPageUsesTemplate Template:EquationRef.
- Kutta–Joukowski_theorem wikiPageUsesTemplate Template:NumBlk.
- Kutta–Joukowski_theorem wikiPageUsesTemplate Template:Refimprove.
- Kutta–Joukowski_theorem wikiPageUsesTemplate Template:Reflist.
- Kutta–Joukowski_theorem subject Category:Aerodynamics.
- Kutta–Joukowski_theorem subject Category:Fluid_dynamics.
- Kutta–Joukowski_theorem subject Category:Physics_theorems.
- Kutta–Joukowski_theorem hypernym Theorem.
- Kutta–Joukowski_theorem type Dynamic.
- Kutta–Joukowski_theorem type Law.
- Kutta–Joukowski_theorem type Mechanic.
- Kutta–Joukowski_theorem type Physic.
- Kutta–Joukowski_theorem type Redirect.
- Kutta–Joukowski_theorem type Theorem.
- Kutta–Joukowski_theorem comment "The Kutta–Joukowski theorem is a fundamental theorem of aerodynamics, that can be used for the calculation of the lift of an airfoil, or of any two-dimensional bodies including circular cylinders, translating in a uniform fluid at a constant speed large enough so that the flow seen in the body-fixed frame is steady and unseparated. The theorem relates the lift generated by an airfoil to the speed of the airfoil through the fluid, the density of the fluid, and the circulation.".
- Kutta–Joukowski_theorem label "Kutta–Joukowski theorem".
- Kutta–Joukowski_theorem sameAs Q1752988.
- Kutta–Joukowski_theorem sameAs Тэарэма_Жукоўскага.
- Kutta–Joukowski_theorem sameAs Satz_von_Kutta-Joukowski.
- Kutta–Joukowski_theorem sameAs Teorema_de_Kutta-Yukovski.
- Kutta–Joukowski_theorem sameAs Kutta–Žukovski-teoreema.
- Kutta–Joukowski_theorem sameAs Théorème_de_Kutta-Jukowski.
- Kutta–Joukowski_theorem sameAs Teorema_di_Kutta-Žukovskij.
- Kutta–Joukowski_theorem sameAs クッタ・ジュコーフスキーの定理.
- Kutta–Joukowski_theorem sameAs Жуковский_теоремасы.
- Kutta–Joukowski_theorem sameAs Teorema_de_Kutta_Joukowski.
- Kutta–Joukowski_theorem sameAs m.02y_8w0.
- Kutta–Joukowski_theorem sameAs Теорема_Жуковского.
- Kutta–Joukowski_theorem sameAs Định_lý_Kutta-Zhukovsky.
- Kutta–Joukowski_theorem sameAs Q1752988.
- Kutta–Joukowski_theorem sameAs 库塔-儒可夫斯基定理.
- Kutta–Joukowski_theorem wasDerivedFrom Kutta–Joukowski_theorem?oldid=694963313.
- Kutta–Joukowski_theorem isPrimaryTopicOf Kutta–Joukowski_theorem.