The concept vortex force in aerodynamics is systematically examined based on a new steady vortex-force theory (Wu et al., Vorticity and vortex dynamics, Springer, 2006) which expresses the aerodynamic force (and moment) by the volume and boundary integrals of the Lamb vector. In this paper, the underlying physics of this theory is explored, including the general role of the Lamb vector in nonlinear aerodynamics, its initial formation, and its relevance to the total-pressure non-uniformity. As a typical example, the theory is applied to the flow over a slender delta wing at a large angle of attack. The highly localized flow structures with high Lamb-vector peaks are identified in terms of their net contribution to various constituents of the...
pp. 65-94) for slender conical bodies and predicted that vortices over a at-plate delta wing at hig...
The problem of mathematically modelling the symmetric vortex pair formed on the lee side of a body ...
<p>Vortex structures are identified by plotting an isosurface of the imaginary part of the complex e...
Recent studies about the Lamb vector have led to the development of the vortex-force theory: a formu...
The unsteady forces acting on a body depend strongly on the local flow structures such as vortices. A...
Some recent developments in the Lamb vector based aerodynamic force breakdown used the concept of vo...
A recently proposed aerodynamic force theory of compressible high Reynolds number flows based on the...
The Lamb vector is known to play a key role in incompressible fluid dynamics and vortex dynamics. In...
The new aerodynamic force theory based on Lamb vector field integration, valid in general for unstea...
A vorticity based theory for the computation and analysis of the aerodynamic force in steady and uns...
An unconventional expression of the aerodynamic force in unsteady viscous flow is pre- sented. It is...
A recently proposed aerodynamic force theory of compressible high-Reynolds-number flows based on the...
Some recent developments in the Lamb-vector-based aerodynamic force breakdown used the concept of vo...
Hot topic of modern Aerodynamics is the analysis of the aerodynamic force. Indeed, the growth in glo...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
pp. 65-94) for slender conical bodies and predicted that vortices over a at-plate delta wing at hig...
The problem of mathematically modelling the symmetric vortex pair formed on the lee side of a body ...
<p>Vortex structures are identified by plotting an isosurface of the imaginary part of the complex e...
Recent studies about the Lamb vector have led to the development of the vortex-force theory: a formu...
The unsteady forces acting on a body depend strongly on the local flow structures such as vortices. A...
Some recent developments in the Lamb vector based aerodynamic force breakdown used the concept of vo...
A recently proposed aerodynamic force theory of compressible high Reynolds number flows based on the...
The Lamb vector is known to play a key role in incompressible fluid dynamics and vortex dynamics. In...
The new aerodynamic force theory based on Lamb vector field integration, valid in general for unstea...
A vorticity based theory for the computation and analysis of the aerodynamic force in steady and uns...
An unconventional expression of the aerodynamic force in unsteady viscous flow is pre- sented. It is...
A recently proposed aerodynamic force theory of compressible high-Reynolds-number flows based on the...
Some recent developments in the Lamb-vector-based aerodynamic force breakdown used the concept of vo...
Hot topic of modern Aerodynamics is the analysis of the aerodynamic force. Indeed, the growth in glo...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
pp. 65-94) for slender conical bodies and predicted that vortices over a at-plate delta wing at hig...
The problem of mathematically modelling the symmetric vortex pair formed on the lee side of a body ...
<p>Vortex structures are identified by plotting an isosurface of the imaginary part of the complex e...