398 research outputs found

    Galactic Outflows and the pollution of the Galactic Environment by Supernovae

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    We here explore the effects of the SN explosions into the environment of star-forming galaxies like the Milky Way. Successive randomly distributed and clustered SNe explosions cause the formation of hot superbubbles that drive either fountains or galactic winds above the galactic disk, depending on the amount and concentration of energy that is injected by the SNe. In a galactic fountain, the ejected gas is re-captured by the gravitational potential and falls back onto the disk. From 3D nonequilibrium radiative cooling hydrodynamical simulations of these fountains, we find that they may reach altitudes up to about 5 kpc in the halo and thus allow for the formation of the so called intermediate-velocity-clouds (IVCs) which are often observed in the halos of disk galaxies. The high-velocity-clouds that are also observed but at higher altitudes (of up to 12 kpc) require another mechanism to explain their production. We argue that they could be formed either by the capture of gas from the intergalactic medium and/or by the action of magnetic fields that are carried to the halo with the gas in the fountains. Due to angular momentum losses to the halo, we find that the fountain material falls back to smaller radii and is not largely spread over the galactic disk. Instead, the SNe ejecta fall nearby the region where the fountain was produced, a result which is consistent with recent chemical models of the galaxy. The fall back material leads to the formation of new generations of molecular clouds and to supersonic turbulence feedback in the disk.Comment: 10 pages, 5 figures; paper of invited talk for the Procs. of the 2007 WISER Workshop (World Space Environment Forum), Alexandria, Egypt, October 2007, Spa. Sci. Rev

    The limiting behavior of solutions to p-Laplacian problems with convection and exponential terms

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    We consider, for a,l1,a,l\geq1, b,s,α>0,b,s,\alpha>0, and p>q1,p>q\geq1, the homogeneous Dirichlet problem for the equation Δpu=λuq1+βua1ub+mtl1eαts-\Delta_{p}u=\lambda u^{q-1}+\beta u^{a-1}\left\vert \nabla u\right\vert ^{b}+mt^{l-1}e^{\alpha t^{s}} in a smooth bounded domain ΩRN.\Omega\subset\mathbb{R}^{N}. We prove that under certain setting of the parameters λ,\lambda, β\beta and mm the problem admits at least one positive solution. Using this result we prove that if λ,β>0\lambda,\beta>0 are arbitrarily fixed and mm is sufficiently small, then the problem has a positive solution up,u_{p}, for all pp sufficiently large. In addition, we show that upu_{p} converges uniformly to the distance function to the boundary of Ω,\Omega, as p.p\rightarrow\infty. This convergence result is new for nonlinearities involving a convection term.Comment: 18 page

    Algorithm for Simulating Atmospheric Turbulence and Aeroelastic Effects on Simulator Motion Systems

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    Atmospheric turbulence produces high frequency accelerations in aircraft, typically greater than the response to pilot input. Motion system equipped flight simulators must present cues representative of the aircraft response to turbulence in order to maintain the integrity of the simulation. Currently, turbulence motion cueing produced by flight simulator motion systems has been less than satisfactory because the turbulence profiles have been attenuated by the motion cueing algorithms. This report presents a new turbulence motion cueing algorithm, referred to as the augmented turbulence channel. Like the previous turbulence algorithms, the output of the channel only augments the vertical degree of freedom of motion. This algorithm employs a parallel aircraft model and an optional high bandwidth cueing filter. Simulation of aeroelastic effects is also an area where frequency content must be preserved by the cueing algorithm. The current aeroelastic implementation uses a similar secondary channel that supplements the primary motion cue. Two studies were conducted using the NASA Langley Visual Motion Simulator and Cockpit Motion Facility to evaluate the effect of the turbulence channel and aeroelastic model on pilot control input. Results indicate that the pilot is better correlated with the aircraft response, when the augmented channel is in place

    Hemodynamic responses during and after multiple sets of stretching exercises performed with and without the Valsalva maneuver

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    OBJECTIVE: This study investigated the acute hemodynamic responses to multiple sets of passive stretching exercises performed with and without the Valsalva maneuver. METHODS: Fifteen healthy men aged 21 to 29 years with poor flexibility performed stretching protocols comprising 10 sets of maximal passive unilateral hip flexion, sustained for 30 seconds with equal intervals between sets. Protocols without and with the Valsalva maneuver were applied in a random counterbalanced order, separated by 48-hour intervals. Hemodynamic responses were measured by photoplethysmography pre-exercise, during the stretching sets, and post-exercise. RESULTS: The effects of stretching sets on systolic and diastolic blood pressure were cumulative until the fourth set in protocols performed with and without the Valsalva maneuver. The heart rate and rate pressure product increased in both protocols, but no additive effect was observed due to the number of sets. Hemodynamic responses were always higher when stretching was performed with the Valsalva maneuver, causing an additional elevation in the rate pressure product. CONCLUSIONS: Multiple sets of unilateral hip flexion stretching significantly increased blood pressure, heart rate, and rate pressure product values. A cumulative effect of the number of sets occurred only for systolic and diastolic blood pressure, at least in the initial sets of the stretching protocols. The performance of the Valsalva maneuver intensified all hemodynamic responses, which resulted in significant increases in cardiac work during stretching exercises

    Detection of lithium plating in li-ion cell anodes using realistic automotive fast-charge profiles

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    The widespread use of electric vehicles is nowadays limited by the “range anxiety” of the customers. The drivers’ main concerns are related to the kilometric range of the vehicle and to the charging time. An optimized fast-charge profile can help to decrease the charging time, without degrading the cell performance and reducing the cycle life. One of the main reasons for battery capacity fade is linked to the Lithium plating phenomenon. This work investigates two methodologies, i.e., three-electrode cell measurement and internal resistance evolution during charging, for detecting the Lithium plating conditions. From this preliminary analysis, it was possible to develop new Multi-Stage Constant-Current profiles, designed to improve the performance in terms of charging time and cells capacity retention with respect to a reference profile. Four new profiles were tested and compared to a reference. The results coming from the new profiles demonstrate a simultaneous improvement in terms of charging time and cycling life, showing the reliability of the implemented methodology in preventing Lithium plating

    Computing the first eigenpair of the p-Laplacian via inverse iteration of sublinear supersolutions

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    We introduce an iterative method for computing the first eigenpair (λp,ep)(\lambda_{p},e_{p}) for the pp-Laplacian operator with homogeneous Dirichlet data as the limit of (μq,uq)(\mu_{q,}u_{q}) as qpq\rightarrow p^{-}, where uqu_{q} is the positive solution of the sublinear Lane-Emden equation Δpuq=μquqq1-\Delta_{p}u_{q}=\mu_{q}u_{q}^{q-1} with same boundary data. The method is shown to work for any smooth, bounded domain. Solutions to the Lane-Emden problem are obtained through inverse iteration of a super-solution which is derived from the solution to the torsional creep problem. Convergence of uqu_{q} to epe_{p} is in the C1C^{1}-norm and the rate of convergence of μq\mu_{q} to λp\lambda_{p} is at least O(pq)O(p-q). Numerical evidence is presented.Comment: Section 5 was rewritten. Jed Brown was added as autho
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