17,776 research outputs found
Turbulent boundary layer over solid and porous surfaces with small roughness
The wind tunnel models and instrumentation used as well as data reduction and error analysis techniques employed are described for an experimental study conducted to measure directly skin friction and obtain profiles of mean velocity, axial and normal turbulence intensity, and Reynolds stress in the untripped boundary on a large diameter axisymmetric body. Results are given for such a body with a (1) smooth, solid surface; (2) a sandpaper roughened, solid surface; (3) a sintered metal, porous surface; (4) a ""smooth'' performated titanium surface; (5) a rough, solid surface made of fine diffusion bonded screening; and (6) a rough, porous surface made of the same screening. The roughness values were in low range (k+ 5 to 7) just above what is normally considered ""hydraulically smooth''. Measurements were taken at several axial locations and tow or normal stream freestream velocities, 45.1 m/sec and 53.5 m/sec
Turbulent boundary layer over solid and porous surfaces with small roughness
Skin friction and profiles of mean velocity, axial and normal turbulence intensity, and Reynolds stress in the untripped boundary layer were measured directly on a large diameter, axisymmetric body with: (1) a smooth, solid surface; (2) a sandpaper-roughened, solid surface; (3) a sintered metal, porous surface; (4) a smooth, perforated titanium surface; (5) a rough solid surface made of fine, diffusion bonded screening, and (6) a rough, porous surface of the same screening. Results obtained for each of these surfaces are discussed. It is shown that a rough, porous wall simply does not influence the boundary layer in the same way as a rough solid wall. Therefore, turbulent transport models for boundary layers over porous surfaces either with or without injection or suction, must include both surface roughness and porosity effects
On the afterglow from the receding jet of gamma-ray burst
According to popular progenitor models of gamma-ray bursts, twin jets should
be launched by the central engine, with a forward jet moving toward the
observer and a receding jet (or the counter jet) moving backwardly. However, in
calculating the afterglows, usually only the emission from the forward jet is
considered. Here we present a detailed numerical study on the afterglow from
the receding jet. Our calculation is based on a generic dynamical description,
and includes some delicate ingredients such as the effect of the equal arrival
time surface. It is found that the emission from the receding jet is generally
rather weak. In radio bands, it usually peaks at a time of d,
with the peak flux nearly 4 orders of magnitude lower than the peak flux of the
forward jet. Also, it usually manifests as a short plateau in the total
afterglow light curve, but not as an obvious rebrightening as once expected. In
optical bands, the contribution from the receding jet is even weaker, with the
peak flux being orders of magnitude lower than the peak flux of the
forward jet. We thus argue that the emission from the receding jet is very
difficult to detect. However, in some special cases, i.e., when the
circum-burst medium density is very high, or if the parameters of the receding
jet is quite different from those of the forward jet, the emission from the
receding jet can be significantly enhanced and may still emerge as a marked
rebrightening. We suggest that the search for receding jet emission should
mostly concentrate on nearby gamma-ray bursts, and the observation campaign
should last for at least several hundred days for each event.Comment: A few citations added, together with a few minor revisions, main
conclusions unchanged, accepted for publication in A&A, 7 figures, 10 Page
Phase diagrams of XXZ model on depleted square lattice
Using quantum Monte Carlo (QMC) simulations and a mean field (MF) theory, we
investigate the spin-1/2 XXZ model with nearest neighbor interactions on a
periodic depleted square lattice. In particular, we present results for 1/4
depleted lattice in an applied magnetic field and investigate the effect of
depletion on the ground state. The ground state phase diagram is found to
include an antiferromagnetic (AF) phase of magnetization and an
in-plane ferromagnetic (FM) phase with finite spin stiffness. The agreement
between the QMC simulations and the mean field theory based on resonating
trimers suggests the AF phase and in-plane FM phase can be interpreted as a
Mott insulator and superfluid of trimer states respectively. While the thermal
transitions of the in-plane FM phase are well described by the
Kosterlitz-Thouless transition, the quantum phase transition from the AF phase
to in-plane FM phase undergo a direct second order insulator-superfluid
transition upon increasing magnetic field.Comment: 7 pages, 8 figures. Revised version, accepted by PRB
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