85 research outputs found

    Asymptotic Steady State Solution to a Bow Shock with an Infinite Mach Number

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    The problem of a cold gas flowing past a stationary object is considered. It is shown that at large distances from the obstacle the shock front forms a parabolic solid of revolution. The interior of the shock front is obtained by solution of the hydrodynamic equations in parabolic coordinates. The results are verified with a hydrodynamic simulation. The drag force and expected spectra are calculated for such shock, both in case of an optically thin and thick media. Finally, relations to astrophysical bow shocks and other analytic works on oblique shocks are discussed

    Atmospheric Mass Loss During Planet Formation: The Importance of Planetesimal Impacts

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    We quantify the atmospheric mass loss during planet formation by examining the contributions to atmospheric loss from both giant impacts and planetesimal accretion. Giant impacts cause global motion of the ground. Using analytic self-similar solutions and full numerical integrations we find (for isothermal atmospheres with adiabatic index (Ξ³=5/3\gamma=5/3) that the local atmospheric mass loss fraction for ground velocities vg<0.25vescv_g < 0.25 v_{esc} is given by Ο‡loss=(1.71vg/vesc)4.9\chi_{loss}=(1.71 v_g/v_{esc})^{4.9}, where vescv_{esc} is the escape velocity from the target. Yet, the global atmospheric mass loss is a weaker function of the impactor velocity vImpv_{Imp} and mass mImpm_{Imp} and given by XlossΒ 0.4x+1.4x2βˆ’0.8x3X_{loss} ~ 0.4x+1.4x^2-0.8x^3 (isothermal atmosphere) and XlossΒ 0.4x+1.8x2βˆ’1.2x3X_{loss} ~ 0.4x+1.8x^2-1.2x^3 (adiabatic atmosphere), where x=(vImpm/vescM)x=(v_{Imp}m/v_{esc}M). Atmospheric mass loss due to planetesimal impacts proceeds in two different regimes: 1) Large enough impactors m>2ρ0(Ο€hR)3/2m > \sqrt{2} \rho_0 (\pi h R)^{3/2} (25~km for the current Earth), are able to eject all the atmosphere above the tangent plane of the impact site, which is h/2Rh/2R of the whole atmosphere, where hh, RR and ρ0\rho_0 are the atmospheric scale height, radius of the target, and its atmospheric density at the ground. 2) Smaller impactors, but above m>4πρ0h3m>4 \pi \rho_0 h^3 (1~km for the current Earth) are only able to eject a fraction of the atmospheric mass above the tangent plane. We find that the most efficient impactors (per unit impactor mass) for atmospheric loss are planetesimals just above that lower limit and that the current atmosphere of the Earth could have resulted from an equilibrium between atmospheric erosion and volatile delivery to the atmosphere from planetesimals. We conclude that planetesimal impacts are likely to have played a major role in atmospheric mass loss over the formation history of the terrestrial planets. (Abridged)Comment: Submitted to Icarus, 39 pages, 16 figure

    Rich: Open Source Hydrodynamic Simulation on a Moving Voronoi Mesh

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    We present here RICH, a state of the art 2D hydrodynamic code based on Godunov's method, on an unstructured moving mesh (the acronym stands for Racah Institute Computational Hydrodynamics). This code is largely based on the code AREPO. It differs from AREPO in the interpolation and time advancement scheme as well as a novel parallelization scheme based on Voronoi tessellation. Using our code we study the pros and cons of a moving mesh (in comparison to a static mesh). We also compare its accuracy to other codes. Specifically, we show that our implementation of external sources and time advancement scheme is more accurate and robust than AREPO's, when the mesh is allowed to move. We performed a parameter study of the cell rounding mechanism (Llyod iterations) and it effects. We find that in most cases a moving mesh gives better results than a static mesh, but it is not universally true. In the case where matter moves in one way, and a sound wave is traveling in the other way (such that relative to the grid the wave is not moving) a static mesh gives better results than a moving mesh. Moreover, we show that Voronoi based moving mesh schemes suffer from an error, that is resolution independent, due to inconsistencies between the flux calculation and change in the area of a cell. Our code is publicly available as open source and designed in an object oriented, user friendly way that facilitates incorporation of new algorithms and physical processes

    Self similar Shocks in Atmospheric Mass Loss due to Planetary Collisions

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    We present a mathematical model for the propagation of the shock waves that occur during planetary collisions. Such collisions are thought to occur during the formation of terrestrial planets, and they have the potential to erode the planet's atmosphere. We show that under certain assumptions, this evolution of the shock wave can be determined using the method of self similar solutions. This self similar solution is of type II, which means that it only applies to a finite region behind the shock front. This region is bounded by the shock front and the sonic point. Energy and matter continuously flow through the sonic point, so that energy in the self similar region is not conserved, as is the case for type I solutions. Instead, the evolution of the shock wave is determined by boundary conditions at the shock front and at the sonic point. We show how the evolution can be determined for different equations of state, allowing these results to be readily used to calculate the atmospheric mass loss from planetary cores made of different materials.Comment: Submitted to Atmosphere special issue "Shock Wave Dynamics and Its Effects on Planetary Atmospheres

    The Signature of a Windy Radio Supernova Progenitor in a Binary System

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    Type II supernova progenitors are expected to emit copious amounts of mass in a dense stellar wind prior to the explosion. When the progenitor is a member of a binary, the orbital motion modulates the density of this wind. When the progenitor explodes, the high-velocity ejecta collides with the modulated wind, which in turn produces a modulated radio signal. In this work we derive general analytic relations between the parameters of the radio signal modulations and binary parameter in the limit of large member mass ratio. We use these relations to infer the semi major axis of SN1979c and a lower bound for the mass of the companion. We further constrain the analytic estimates by numerical simulations using the AMUSE framework. In these calculations we simulate the progenitor binary system including the wind and the gravitational effect of a companion star. The simulation output is compared to the observed radio signal in supernova SN1979C. We find that it must have been a binary with an orbital period of about 2000 year. If the exploding star evolved from a ∼18MβŠ™\sim 18 M_{\odot} zero-age main-sequence at solar metalicity, we derive a companion mass of 55 to 12MβŠ™12 M_{\odot} in an orbit with an eccentricity lower than about 0.8
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