Similarities between Lift (force) and Lifting-line theory
Lift (force) and Lifting-line theory have 10 things in common (in Unionpedia): Airfoil, Angle of attack, Chord (aeronautics), Circulation (fluid dynamics), Fluid dynamics, Kutta–Joukowski theorem, Lift coefficient, Lift-induced drag, Navier–Stokes equations, Vortex.
Airfoil
An airfoil (American English) or aerofoil (British English) is the shape of a wing, blade (of a propeller, rotor, or turbine), or sail (as seen in cross-section).
Airfoil and Lift (force) · Airfoil and Lifting-line theory ·
Angle of attack
In fluid dynamics, angle of attack (AOA, or \alpha (Greek letter alpha)) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is moving.
Angle of attack and Lift (force) · Angle of attack and Lifting-line theory ·
Chord (aeronautics)
In aeronautics, chord refers to the imaginary straight line joining the leading and trailing edges of an aerofoil.
Chord (aeronautics) and Lift (force) · Chord (aeronautics) and Lifting-line theory ·
Circulation (fluid dynamics)
In fluid dynamics, circulation is the line integral around a closed curve of the velocity field.
Circulation (fluid dynamics) and Lift (force) · Circulation (fluid dynamics) and Lifting-line theory ·
Fluid dynamics
In physics and engineering, fluid dynamics is a subdiscipline of fluid mechanics that describes the flow of fluids - liquids and gases.
Fluid dynamics and Lift (force) · Fluid dynamics and Lifting-line theory ·
Kutta–Joukowski theorem
The Kutta–Joukowski theorem is a fundamental theorem in aerodynamics used for the calculation of lift of an airfoil and 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.
Kutta–Joukowski theorem and Lift (force) · Kutta–Joukowski theorem and Lifting-line theory ·
Lift coefficient
The lift coefficient (CL, CN or Cz) is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Lift (force) and Lift coefficient · Lift coefficient and Lifting-line theory ·
Lift-induced drag
In aerodynamics, lift-induced drag, induced drag, vortex drag, or sometimes drag due to lift, is an aerodynamic drag force that occurs whenever a moving object redirects the airflow coming at it.
Lift (force) and Lift-induced drag · Lift-induced drag and Lifting-line theory ·
Navier–Stokes equations
In physics, the Navier–Stokes equations, named after Claude-Louis Navier and George Gabriel Stokes, describe the motion of viscous fluid substances.
Lift (force) and Navier–Stokes equations · Lifting-line theory and Navier–Stokes equations ·
Vortex
In fluid dynamics, a vortex (plural vortices/vortexes) is a region in a fluid in which the flow revolves around an axis line, which may be straight or curved.
The list above answers the following questions
- What Lift (force) and Lifting-line theory have in common
- What are the similarities between Lift (force) and Lifting-line theory
Lift (force) and Lifting-line theory Comparison
Lift (force) has 122 relations, while Lifting-line theory has 26. As they have in common 10, the Jaccard index is 6.76% = 10 / (122 + 26).
References
This article shows the relationship between Lift (force) and Lifting-line theory. To access each article from which the information was extracted, please visit: