Finite domain viscous correction to the Kutta-Joukowski Theorem in incompressible flow

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

The classical relationship between lift and circulation in inviscid and irrotational flow was developed independently. Although being derived from ideal-fluid considerations with a free-slip (inviscid) boundary condition on the lifting airfoil, the Kutta Joukowski theorem has proven its applicability to high-Reynolds-number attached viscous flow, and constitutes the foundation of human understanding of aerodynamic lift. A recently published review on the development of circulation theory during the first three decades of the last century describes in some detail the complex discussions among the various experts at that time, some of whom were in favor and some opposing the circulation theory. In viscous flow, the circulation results from the vorticity generated on the no-slip wall of the airfoil. This vorticity is present throughout the wake, and subject to stretching and diffusion.

Original languageEnglish (US)
Pages (from-to)2079-2083
Number of pages5
JournalAIAA Journal
Volume52
Issue number9
DOIs
StatePublished - Jan 1 2014

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Incompressible flow
Viscous flow
Vorticity
Airfoils
Stretching
Aerodynamics
Reynolds number
Boundary conditions
Fluids

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

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abstract = "The classical relationship between lift and circulation in inviscid and irrotational flow was developed independently. Although being derived from ideal-fluid considerations with a free-slip (inviscid) boundary condition on the lifting airfoil, the Kutta Joukowski theorem has proven its applicability to high-Reynolds-number attached viscous flow, and constitutes the foundation of human understanding of aerodynamic lift. A recently published review on the development of circulation theory during the first three decades of the last century describes in some detail the complex discussions among the various experts at that time, some of whom were in favor and some opposing the circulation theory. In viscous flow, the circulation results from the vorticity generated on the no-slip wall of the airfoil. This vorticity is present throughout the wake, and subject to stretching and diffusion.",
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Finite domain viscous correction to the Kutta-Joukowski Theorem in incompressible flow. / Schmitz, Sven.

In: AIAA Journal, Vol. 52, No. 9, 01.01.2014, p. 2079-2083.

Research output: Contribution to journalArticle

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