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

Abstract

Here, this paper introduces an algorithm that determines the thermodynamic conditions behind incident and reflectedshocksinaerosol-ladenflows.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 exper- imental uncertainties

Authors:
ORCiD logo [1];  [2];  [3];  [3]
  1. Sandia National Lab. (SNL-CA), Livermore, CA (United States)
  2. Lawrence Livermore National Lab. (LLNL), Livermore, CA (United States)
  3. Stanford Univ., CA (United States)
Publication Date:
Research Org.:
Sandia National Lab. (SNL-CA), Livermore, CA (United States); Lawrence Livermore National Lab. (LLNL), Livermore, CA (United States)
Sponsoring Org.:
USDOE National Nuclear Security Administration (NNSA); USDOE Office of Science (SC), Basic Energy Sciences (BES) (SC-22); USDOE Office of Science (SC), Basic Energy Sciences (BES) (SC-22). Chemical Sciences, Geosciences & Biosciences Division
OSTI Identifier:
1338395
Alternate Identifier(s):
OSTI ID: 1458673
Report Number(s):
SAND-2016-12712J; LLNL-JRNL-735751
Journal ID: ISSN 0938-1287; 649986
Grant/Contract Number:  
AC04-94AL85000; AC52-07NA27344
Resource Type:
Accepted Manuscript
Journal Name:
Shock Waves
Additional Journal Information:
Journal Volume: 26; Journal Issue: 4; Journal ID: ISSN 0938-1287
Publisher:
Springer
Country of Publication:
United States
Language:
English
Subject:
02 PETROLEUM; Shock tube; Aerosol; Evaporation; Diesel fuel; Engineering - Mechanical and civil engineering, Chemistry - Inorganic, organic, physical and analytical chemistry, Chemistry, Mathematics and Computing, Energy - Biomass, Energy - Synthetic fuels

Citation Formats

Campbell, Matthew Frederick, Haylett, D. R., Davidson, D. F., and Hanson, R. K. AEROFROSH: a shock condition calculator for multi-component fuel aerosol-laden flows. United States: N. p., 2015. Web. doi:10.1007/s00193-015-0582-3.
Campbell, Matthew Frederick, Haylett, D. R., Davidson, D. F., & Hanson, R. K. AEROFROSH: a shock condition calculator for multi-component fuel aerosol-laden flows. United States. doi:10.1007/s00193-015-0582-3.
Campbell, Matthew Frederick, Haylett, D. R., Davidson, D. F., and Hanson, R. K. Tue . "AEROFROSH: a shock condition calculator for multi-component fuel aerosol-laden flows". United States. doi:10.1007/s00193-015-0582-3. https://www.osti.gov/servlets/purl/1338395.
@article{osti_1338395,
title = {AEROFROSH: a shock condition calculator for multi-component fuel aerosol-laden flows},
author = {Campbell, Matthew Frederick and Haylett, D. R. and Davidson, D. F. and Hanson, R. K.},
abstractNote = {Here, this paper introduces an algorithm that determines the thermodynamic conditions behind incident and reflectedshocksinaerosol-ladenflows.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 exper- imental uncertainties},
doi = {10.1007/s00193-015-0582-3},
journal = {Shock Waves},
number = 4,
volume = 26,
place = {United States},
year = {2015},
month = {8}
}

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