Observing turbulent fragmentation in simulations: predictions for CARMA and ALMA
نویسندگان
چکیده
منابع مشابه
CO Line Emission from Lyman Break Galaxies – Cosmological Simulations and Predictions for ALMA
We present maps and spectra of rotational CO line emission from a cosmological self-consistent N-body/hydrodynamical TreeSPH simulation of a z ∼ 3 merger system with properties similar to Lyman Break Galaxies at those redshifts. The CO line intensities and widths predicted by our simulation are in good agreement with those of MS1512−cB58 – the only Lyman break system detected in CO to date. We ...
متن کاملObserving Extrasolar Planetary Systems with ALMA
We address in this white paper the ability of ALMA to observe extrasolar planetary systems (in various stages of formation). The observation of extrasolar planetary systems is thought to be one of the most important science drivers for ALMA. As such, we should have some idea of what the capabilities might be in this regard.
متن کاملObserving Baryonic Dark Matter with ALMA
It has recently been argued that the unidentified SCUBA objects (USOs) are a thick disk population of free-floating dense, compact galactic gas clumps at a temperature of about 7 K. The characteristic mass scale is constrained to be on the order of a Jupiter mass, and the size is about 10 AU. A typical galactic USO is located at a distance from the sun of about 300 pc. We have calculated the mo...
متن کاملObserving Stars & Extrasolar Planetary Systems with ALMA
We address in this memo the ability of ALMA to observe stars and extrasolar planetary systems (in various stages of formation). The observation of extrasolar planetary systems is thought to be one of the most important science drivers for ALMA. As such, we should have some idea of what the capabilities might be in this regard. In addition, ALMA will be the first instrument which will be able to...
متن کاملLaminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow
In the present work, an engineering method is developed to predict laminar and turbulent heating-rate solutions for blunt reentry spacecraft at hypersonic conditions. The calculation of aerodynamic heating around blunt bodies requires alternative solution of inviscid flow field around the hypersonic bodies. In this paper, the procedure is of an inverse nature, that is, a shock wave is assumed a...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Monthly Notices of the Royal Astronomical Society: Letters
سال: 2011
ISSN: 1745-3925
DOI: 10.1111/j.1745-3933.2011.01194.x