2023
DOI: 10.1186/s42774-023-00143-3
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Can lift be generated in a steady inviscid flow?

Abstract: This paper presents a critical evaluation of the physical aspects of lift generation to prove that no lift can be generated in a steady inviscid flow. Hence, the answer to the recurring question in the paper title is negative. In other words, the fluid viscosity is necessary in lift generation. The relevant topics include D’Alembert’s paradox of lift and drag, the Kutta condition, the force expression based on the boundary enstrophy flux (BEF), the vortex lift, and the generation of the vorticity and circulati… Show more

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Cited by 5 publications
(2 citation statements)
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“…To construct the model, we recognize that although the fundamental origins of lift and drag on an aerodynamic body immersed in an airflow are still subject to debate (Regis, 2020;Gonzalez and Taha, 2022;Liu, 2023), the resulting expressions for forces and torques on the body are simple (especially in the non-stall regime), and those alone are sufficient to yield the dynamics of a single aircraft flying in isolation. For simplicity, we restrict ourselves to two-dimensional motions in the pitch plane or longitudinal plane.…”
Section: Symbol Significancementioning
confidence: 99%
“…To construct the model, we recognize that although the fundamental origins of lift and drag on an aerodynamic body immersed in an airflow are still subject to debate (Regis, 2020;Gonzalez and Taha, 2022;Liu, 2023), the resulting expressions for forces and torques on the body are simple (especially in the non-stall regime), and those alone are sufficient to yield the dynamics of a single aircraft flying in isolation. For simplicity, we restrict ourselves to two-dimensional motions in the pitch plane or longitudinal plane.…”
Section: Symbol Significancementioning
confidence: 99%
“…One such assumption is to neglect the viscosity term of the Navier-Stokes equations, which yields Euler's equations. In aerodynamics, the main effect of viscosity is to create a thin Boundary Layer (BL) on all lifting and non-lifting surfaces (Liu, 2021(Liu, , 2023, and neglecting it will lead to inaccurate where p is fluid film pressure, 𝑥 and 𝑦 is the bearing width and length coordinates, ℎ is the fluid film thickness, µ is fluid viscosity, ρ is the fluid density, 𝑢, 𝑣, 𝜔 are the bounding body velocities in 𝑥, 𝑦, 𝑧 respectively, and 𝑎, 𝑏 are subscripts denoting the top and bottom bounding bodies respectively.…”
Section: The Navier-stokes Equationsmentioning
confidence: 99%