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  2. Lift (force) - Wikipedia

    en.wikipedia.org/wiki/Lift_(force)

    The lift force frequency is characterised by ... The above lift equation neglects the ... [96] Lift is generated in accordance with the fundamental principles ...

  3. Lifting-line theory - Wikipedia

    en.wikipedia.org/wiki/Lifting-line_theory

    Lifting line theory supposes wings that are long and thin with negligible fuselage, akin to a thin bar (the eponymous "lifting line") of span 2s driven through the fluid. . From the Kutta–Joukowski theorem, the lift L(y) on a 2-dimensional segment of the wing at distance y from the fuselage is proportional to the circulation Γ(y) about the bar a

  4. Kutta–Joukowski theorem - Wikipedia

    en.wikipedia.org/wiki/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 body including circular cylinders) translating in a uniform fluid at a constant speed so large that the flow seen in the body-fixed frame is steady and unseparated.

  5. Bernoulli's principle - Wikipedia

    en.wikipedia.org/wiki/Bernoulli's_principle

    Bernoulli's principle can be used to calculate the lift force on an airfoil, if the behaviour of the fluid flow in the vicinity of the foil is known. For example, if the air flowing past the top surface of an aircraft wing is moving faster than the air flowing past the bottom surface, then Bernoulli's principle implies that the pressure on the ...

  6. Wind-turbine aerodynamics - Wikipedia

    en.wikipedia.org/wiki/Wind-turbine_aerodynamics

    The force vector is not straightforward, as stated earlier there are two types of aerodynamic forces, lift and drag. Accordingly, there are two non-dimensional parameters. However, both variables are non-dimensionalized in a similar way. The formula for lift is given below, the formula for drag is given after:

  7. Lift coefficient - Wikipedia

    en.wikipedia.org/wiki/Lift_coefficient

    The section lift coefficient is based on two-dimensional flow over a wing of infinite span and non-varying cross-section so the lift is independent of spanwise effects and is defined in terms of ′, the lift force per unit span of the wing. The definition becomes

  8. Scientists Are on the Brink of Discovering the Fifth ... - AOL

    www.aol.com/scientists-brink-discovering-fifth...

    Scientists Close to Finding 5th Fundamental Force tmeks - Getty Images. Researchers may be on the brink of discovering evidence of a fifth fundamental force. As far as we know, at the most basic ...

  9. Euler equations (fluid dynamics) - Wikipedia

    en.wikipedia.org/wiki/Euler_equations_(fluid...

    The Hugoniot equation, coupled with the fundamental equation of state of the material: e = e ( v , p ) , {\displaystyle e=e(v,p),} describes in general in the pressure volume plane a curve passing by the conditions (v 0 , p 0 ), i.e. the Hugoniot curve , whose shape strongly depends on the type of material considered.