2,196 research outputs found
Quantum affine vertex algebras associated to untwisted quantum affinization algebras
Let be the untwisted quantum
affinization of a symmetrizable quantum Kac-Moody algebra . For , we construct an -adic
quantum vertex algebra , and establish a
one-to-one correspondence between -coordinated -modules and restricted -modules of level . Suppose that is a positive integer. We
construct a quotient -adic quantum vertex algebra of , and establish a
one-to-one correspondence between certain -coordinated -modules and restricted integrable -modules of level . Suppose further that
is of finite type. We prove that is isomorphic to
the simple affine vertex algebra
Millimeter line observations toward four local galaxies
We present results of millimeter line observations toward four local gas-rich
galaxies (NGC 3079, NGC 4258, NGC 6240 and VII Zw 31) with the IRAM 30 meter
millimeter telescope. More than 33 lines in these four sources were detected,
including normal dense gas tracers (HCN 1-0, HCO 1-0, and CH 1-0, etc)
and their isotopic species. HCN (1-0) and HCO (1-0) are
detected for the first time in NGC 4258. Optical depths of HCN 1-0 and
HCO 1-0 were estimated with detected isotopic lines in NGC 4258, which
were 4.1 and 2.6, respectively. HCN , which requires high volume
density and high temperature to excite, was detected in NGC 6240. High ratios
of HCO/HCN in NGC 4258 and NGC 6240 imply that this ratio might not be a
perfect diagnostic tool between AGN and starburst environments, due to
contamination/combination of both processes. The low HCN/HCN line ratios
with less than 0.15 in NGC 4258, NGC 6240 and the non-detection of HCN line
in NGC 3079 and VII Zw 31 indicates that these four galaxies are HCN-poor
galaxies. The variation of fractional abundance of CN in different types of
galaxies is large.Comment: 15pages, 13 figures; accepted for publication in MNRA
Experimental Study on the Thermodynamic Damage Power of Ammunition Deflagration in a Closed Explosive Device
The high temperature and high pressure gas produced by propellant deburning has strong thermal effect,which will produce strong thermal damage effect on the target. In this study, an improved closed explosive device was used to simulate the thermal shock loading of 5/7 single base propellant with a charge mass of 17.4 g, and the change law of heat flow density of propellant in the process of deflagration in a closed environment was tested. The experimental results show that the temperature rises rapidly during the deflagration of the 5/7 single-base propellant, and the maximum heat flow density can reach 17.68 MW/ m2 . The curves obtained from the three tests have good consistency in the change trend, which proves the engineering practicability of the improved closed explosive device in the study
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