AEROFROSH: a shock condition calculator for multi-component fuel aerosol-laden flows

被引：42
作者：
Campbell, M. F. [1 ]
Haylett, D. R. [2 ]
Davidson, D. F. [3 ]
Hanson, R. K. [3 ]
机构：
[1] Sandia Natl Labs, Livermore, CA 94551 USA
[2] Lawrence Livermore Natl Lab, Livermore, CA 94551 USA
[3] Stanford Univ, Stanford, CA 94305 USA
来源：
SHOCK WAVES | 2016年 / 26卷 / 04期
关键词：
Shock tube; Aerosol; Evaporation; Diesel fuel; IGNITION DELAY TIMES; VAPOR-DROPLET FLOWS; RELAXATION ZONE; WATER DROPLETS; COMPRESSIBLE FLOWS; PHASE-TRANSITION; DIESEL IGNITION; PRESSURE FUELS; METHYL OLEATE; DUSTY GASES;
D O I：
10.1007/s00193-015-0582-3
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
This article introduces an algorithm that determines the thermodynamic conditions behind incident and reflected shocks in aerosol-laden flows. Importantly, the algorithm accounts for the effects of droplet evaporation on post-shock properties. Additionally, this article describes an algorithm for resolving the effects of multiple-component-fuel droplets. This article presents the solution methodology and compares the results to those of another similar shock calculator. It also provides examples to show the impact of droplets on post-shock properties and the impact that multi-component fuel droplets have on shock experimental parameters. Finally, this paper presents a detailed uncertainty analysis of this algorithm's calculations given typical experimental uncertainties.
引用
收藏
页码：429 / 447
页数：19
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