Some properties of the ideal Ginzburg–Landau vortex lattice

2004 ◽  
Vol 404 (1-4) ◽  
pp. 74-77 ◽  
Author(s):  
E.H. Brandt
2005 ◽  
Vol 19 (01n03) ◽  
pp. 435-437
Author(s):  
ERNST HELMUT BRANDT
Keyword(s):  

Some properties of the ideal and pinned vortex lattice in superconductors are outlined.


2012 ◽  
Vol 313 (3) ◽  
pp. 635-743 ◽  
Author(s):  
Etienne Sandier ◽  
Sylvia Serfaty

2020 ◽  
Vol 498 (1) ◽  
pp. 304-309
Author(s):  
Lev B Leinson

ABSTRACT In the Ginzburg–Landau limit, a possible texture without singular cores in a rotating neutron spin-triplet superfluid is studied. The lattice of non-singular vortices is constructed with a vorticity diffusely distributed over the entire unit cell. The upper limit of the free energy associated with this structure is estimated, and the result shows that non-singular vortices are more preferable in the core of rotating neutron stars than ordinary linear singular vortices. The order parameter of the studied neutron system belongs to the unitary class. This implies that the superfluid under consideration does not have spin polarization and the core-less 3P2 vortices do not have magnetization, which makes electron scattering by vortices ineffective. For the same reason, pinning with flux tubes is also suppressed. This can affect the hydrodynamics of superfluid neutron stars.


2012 ◽  
Vol 14 (04) ◽  
pp. 1250027 ◽  
Author(s):  
SYLVIA SERFATY ◽  
IAN TICE

In this paper we obtain optimal estimates for the "currents" associated to point masses in the plane, in terms of the Coulombian renormalized energy of Sandier–Serfaty [From the Ginzburg–Landau model to vortex lattice problems, to appear in Comm. Math. Phys. (2012); One-dimensional log gases and the renormalized energy, in preparation]. To derive the estimates, we use a technique that we introduced in [Lorentz space estimates for the Ginzburg–Landau energy, J. Funct. Anal. 254(3) (2008) 773–825], which couples the "ball construction method" to estimates in the Lorentz space L2,∞.


2020 ◽  
Vol 14 (2) ◽  
pp. 268-272
Author(s):  
Jemitola O. Paul ◽  
Okafor E. Gabriel ◽  
Godwin Abbe

Background: Induced drag accounts for significant percentage of cruise and total aircraft drag. In agreement with Prandtl’s theorem, the ideal arrangement for minimum induced drag is a closed biplane design. Past studies have implemented fixed tip fins for closed biplane design, with the reduction of induced drag associated with fixed tip fin found to be less than optimal. A review of patents related to the box-wing aircraft was carried out. Methods: In an attempt to further reduce the induced drag for box wing aircraft, this study proposed the implementation of Active Tip Fins (ATF) for aircraft design. Athena Vortex Lattice (AVL) software was used to simulate the induced drag associated with AFT in comparison with that of a fixed tip fin. Results: From the result, the ATF design shows a superior induced drag reduction. Conclusion: ATF design is a novel concept that has the potential of improving box wing aircraft performance.


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