60,508 research outputs found
Vapor liquid separator Patent
Vapor-liquid separator design with vapor driven pump for separated liquid pumping for application in propellant transfe
Automatically deploying nozzle exit cone extension Patent
Automatically deploying nozzle exit cone extensio
SCUBA observations of the Horsehead Nebula - what did the horse swallow?
We present observations taken with SCUBA on the JCMT of the Horsehead Nebula
in Orion (B33), at wavelengths of 450 and 850 \mum. We see bright emission from
that part of the cloud associated with the photon-dominated region (PDR) at the
`top' of the horse's head, which we label B33-SMM1. We characterise the
physical parameters of the extended dust responsible for this emission, and
find that B33-SMM1 contains a more dense core than was previously suspected. We
compare the SCUBA data with data from the Infrared Space Observatory (ISO) and
find that the emission at 6.75-\mum is offset towards the west, indicating that
the mid-infrared emission is tracing the PDR while the submillimetre emission
comes from the molecular cloud core behind the PDR. We calculate the virial
balance of this core and find that it is not gravitationally bound but is being
confined by the external pressure from the HII region IC434, and that it will
either be destroyed by the ionising radiation, or else may undergo triggered
star formation. Furthermore we find evidence for a lozenge-shaped clump in the
`throat' of the horse, which is not seen in emission at shorter wavelengths. We
label this source B33-SMM2 and find that it is brighter at submillimetre
wavelengths than B33-SMM1. SMM2 is seen in absorption in the 6.75-\mum ISO
data, from which we obtain an independent estimate of the column density in
excellent agreement with that calculated from the submillimetre emission. We
calculate the stability of this core against collapse and find that it is in
approximate gravitational virial equilibrium. This is consistent with it being
a pre-existing core in B33, possibly pre-stellar in nature, but that it may
also eventually undergo collapse under the effects of the HII region.Comment: 11 pages, 6 figures, accepted by MNRA
Modelling submillimetre spectra of the protostellar infall candidates NGC1333-IRAS2 and Serpens SMM4
We present a radiative transfer model, which is applicable to the study of
submillimetre spectral line observations of protostellar envelopes. The model
uses an exact, non-LTE, spherically symmetric radiative transfer `Stenholm'
method, which numerically solves the radiative transfer problem by the process
of `Lambda-iteration'. We also present submillimetre spectral line data of the
Class 0 protostars NGC1333-IRAS2 and Serpens SMM4. We examine the physical
constraints which can be used to limit the number and range of parameters used
in protostellar envelope models, and identify the turbulent velocity and tracer
molecule abundance as the principle sources of uncertainty in the radiative
transfer modelling. We explore the trends in the appearance of the predicted
line profiles as key parameters in the models are varied.
We find that the separation of the two peaks of a typical infall profile is
dependent not on the evolutionary status of the collapsing protostar, but on
the turbulent velocity dispersion in the envelope. We also find that the line
shapes can be significantly altered by rotation.
Fits are found for the observed line profiles of IRAS2 and SMM4 using
plausible infall model parameters. The density and velocity profiles in our
best fit models are inconsistent with a singular isothermal sphere model. We
find better agreement with a form of collapse which assumes non-static initial
conditions. We also find some evidence that the infall velocities are retarded
from free-fall towards the centre of the cloud, probably by rotation, and that
the envelope of SMM4 is rotationally flattened.Comment: Accepted by MNRA
A simple model for the short-time evolution of near-surface current and temperature profiles
A simple analytical/numerical model has been developed for computing the
evolution, over periods of up to a few hours, of the current and temperature
profile in the upper layer of the ocean. The model is based upon conservation
laws for heat and momentum, and employs an eddy diffusion parameterisation
which is dependent on both the wind speed and the wind stress applied at the
sea surface. Other parameters such as the bulk-skin surface temperature
difference and CO flux are determined by application of the Molecular
Oceanic Boundary Layer Model (MOBLAM) of Schluessel and Soloviev. A similar
model, for the current profile only, predicts a temporary increase in wave
breaking intensity and decrease in wave height under conditions where the wind
speed increases suddenly, such as, for example, during gusts and squalls. The
model results are compared with measurements from the lagrangian Skin Depth
Experimental Profiler (SkinDeEP) surface profiling instrument made during the
1999 MOCE-5 field experiment in the waters around Baja California. SkinDeEP
made repeated profiles of temperature within the upper few metres of the water
column. Given that no tuning was performed in the model, and that the model
does not take account of stratification, the results of the model runs are in
rather good agreement with the observations. The model may be suitable as an
interface between time-independent models of processes very near the surface,
and larger-scale three-dimensional time-dependent ocean circulation models. A
straightforward extension of the model should also be suitable for making
time-dependent computations of gas concentration in the near-surface layer of
the ocean.Comment: 20 pages, 5 figures, 1 table. In press at Deep-Sea Research II. Uses
a modified form of elsart.cls. Proof correction
Aeroplane design study STOL airliner (A71). Part 1- configuration description and data
The interest in STOL airliners was reflected in the
choice of a 100-118 passenger short range aircraft of this
type as the 1971 design project. In addition to the use of
the study for detailed investigation by the students of
Aircraft Design it also served as the basis for an
investigation of the low speed lift and control problems
of STOL aircraft.
This report is concerned with a description of the
configuration adopted and specification of geometric and
aerodynamic data. As such it is the first part of the
complete reporting of the investigation, subsequent parts
being concerned with the more detailed work.
The aircraft was designed to operate from 2000 ft long
single runways and have a cruising speed of up to 11 - 0.83
at 30,000 ft altitude. The estimated gross weight is
115,000 lb and when landing at 100,000 lb weight the approach
speed is 79 knots. The high lift coefficients necessitated
by this are obtained either by externally blown jet flaps or
an augmenter wing arrangement
SCUBA polarisation observations of the magnetic fields in the prestellar cores L1498 and L1517B
We have mapped linearly polarized dust emission from the prestellar cores
L1498 and L1517B with the James Clerk Maxwell Telescope (JCMT) using the
Submillimetre Common User Bolometer Array (SCUBA) and its polarimeter SCUBAPOL
at a wavelength of 850um. We use these measurements to determine the
plane-of-sky magnetic field orientation in the cores. In L1498 we see a
magnetic field across the peak of the core that lies at an offset of 19 degrees
to the short axis of the core. This is similar to the offsets seen in previous
observations of prestellar cores. To the southeast of the peak, in the
filamentary tail of the core, we see that the magnetic field has rotated to lie
almost parallel to the long axis of the filament. We hypothesise that the field
in the core may have decoupled from the field in the filament that connects the
core to the rest of the cloud. We use the Chandrasekhar-Fermi (CF) method to
measure the plane-of-sky field strength in the core of L1498 to be 10 +/- 7 uG.
In L1517B we see a more gradual turn in the field direction from the northern
part of the core to the south. This appears to follow a twist in the filament
in which the core is buried, with the field staying at a roughly constant 25
degree offset to the short axis of the filament, also consistent with previous
observations of prestellar cores. We again use the CF method and calculate the
magnetic field strength in L1517B also to be 30 +/- 10 uG. Both cores appear to
be roughly virialised. Comparison with our previous work on somewhat denser
cores shows that, for the denser cores, thermal and non-thermal (including
magnetic) support are approximately equal, while for the lower density cores
studied here, thermal support dominates.Comment: 6 pages, 2 figures; accepted for publication by MNRA
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