95,345 research outputs found
An improvement in blackbody cavity design
Setting the axis of the conical cavity at an angle to the axis of observation removes the imperfection at the apex of the cone from the direct observation area of the radiometer. Fillet no longer behaves as a nonuniformity in the blackbody
Bosonic Preheating in Left-Right-Symmetric SUSY GUTs
We investigate the possibility of a bosonic preheating in the simplest model
of supersymmetric Hybridinflation (F-term inflation), which was considered
first by Dvali et al. Here the inflationary superpotential is of the
O'Raifertaigh-Witten type. The end of inflation is related to a non-thermal
phase transition, which in the context of left-right symmetric models lowers
the rank of the gauge group. Using the homogeneous classical field ansatz for
the appearing condensates, our results indicate that the parametric creation of
bosonic particles does not occure in the model under consideration.Comment: 14 pages, 6 figure
Aluminium oxide in the optical spectrum of VY Canis Majoris
We report the first identification of the optical bands of the B-X system of
AlO in the red supergiant VY CMa. In addition to TiO, VO, ScO, and YO, which
were recognized in the optical spectrum of the star long time ago, AlO is
another refractory molecule which displays strong emission bands in this
peculiar star. Simulating the bands of AlO, we derive a rotational temperature
of the circumstellar gas of Trot=700K. By resolving individual rotational
components of the bands, we derive the kinematical characteristics of the gas,
finding that the emission is centered at the stellar radial velocity and its
intrinsic width is 13.5 km/s (full width at half maximum). It is the narrowest
emission among all (thermal) features observed in VY CMa so far. The
temperature and line widths suggest that the emission arises in gas located
within ~20 stellar radii, where the outflow is still being accelerated. This
result contradicts equilibrium-chemistry models which predict substantial AlO
abundances only to within a few stellar radii. We argue that non-equilibrium
models involving propagation of shocks are needed to explain the observations.Comment: to appear in A&
Cluster: A fleet of four spacecraft to study plasma structures in three dimensions
The four Cluster spacecraft are spin stabilized spacecraft which are designed and built under stringent requirements as far as electromagnetic cleanliness is concerned. Conductive surfaces and low electromagnetic background noise are mandatory for accurate electric field and cold plasma measurements. The mission is implemented in collaboration between ESA and NASA. A Russian mission will be closely coordinated with Cluster
Spin Effects in the Local Density of States of GaAs
We present spin-resolved measurements of the local density of states in Si
doped GaAs. Both spin components exhibit strong mesoscopic fluctuations. In the
magnetic quantum limit, the main features of the spin-up and spin-down
components of the local density of states are found to be identical apart from
Zeeman splitting. Based on this observation, we introduce a mesoscopic method
to measure the -factor in a material where macroscopic methods are severely
restricted by disorder. Differences between the spin-up and spin-down
components are discussed in terms of spin relaxation due to spin-orbit
coupling.Comment: 4 pages and 5 figure
Analysis of flexible aircraft longitudinal dynamics and handling qualities. Volume 2: Data
Two analysis methods are applied to a family of flexible aircraft in order to investigate how and when structural (especially dynamic aeroelastic) effects affect the dynamic characteristics of aircraft. The first type of analysis is an open loop modal analysis technique. This method considers the effect of modal residue magnitudes on determining vehicle handling qualities. The second method is a pilot in the loop analysis procedure that considers several closed loop system characteristics. Both analyses indicated that dynamic aeroelastic effects caused a degradation in vehicle tracking performance, based on the evaluation of some simulation results. Volume 2 consists of the presentation of the state variable models of the flexible aircraft configurations used in the analysis applications mode shape plots for the structural modes, numerical results from the modal analysis frequency response plots from the pilot in the loop analysis and a listing of the modal analysis computer program
Crater size estimates for large-body terrestrial impact
Calculating the effects of impacts leading to global catastrophes requires knowledge of the impact process at very large size scales. This information cannot be obtained directly but must be inferred from subscale physical simulations, numerical simulations, and scaling laws. Schmidt and Holsapple presented scaling laws based upon laboratory-scale impact experiments performed on a centrifuge (Schmidt, 1980 and Schmidt and Holsapple, 1980). These experiments were used to develop scaling laws which were among the first to include gravity dependence associated with increasing event size. At that time using the results of experiments in dry sand and in water to provide bounds on crater size, they recognized that more precise bounds on large-body impact crater formation could be obtained with additional centrifuge experiments conducted in other geological media. In that previous work, simple power-law formulae were developed to relate final crater diameter to impactor size and velocity. In addition, Schmidt (1980) and Holsapple and Schmidt (1982) recognized that the energy scaling exponent is not a universal constant but depends upon the target media. Recently, Holsapple and Schmidt (1987) includes results for non-porous materials and provides a basis for estimating crater formation kinematics and final crater size. A revised set of scaling relationships for all crater parameters of interest are presented. These include results for various target media and include the kinematics of formation. Particular attention is given to possible limits brought about by very large impactors
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