A shock tube study of jet fuel pyrolysis and ignition at elevated pressures and temperatures-Reference-Cited by-同舟云学术

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A shock tube study of jet fuel pyrolysis and ignition at elevated pressures and temperatures

Published:2018-08 Issue: Volume:226 Page:338-344
ISSN:0016-2361
Container-title:Fuel
language:en
Short-container-title:Fuel

Author:

Shao Jiankun^ORCID,Zhu Yangye,Wang Shengkai^ORCID,Davidson David F.,Hanson Ronald K.

Funder

Air Force Office of Scientific Research through AFOSR

US Federal Aviation Administration (FAA) Office of Environment and Energy

Publisher

Elsevier BV

Subject

Organic Chemistry,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference16 articles.

1. Shock tube determination of ignition delay times in full-blend and surrogate fuel mixtures;Gauthier;Combust Flame,2004

2. Experimental data and kinetic modeling of primary reference fuel mixtures;Callahan;Proc Combust Inst,1996

3. A reduced chemical kinetic model for IC engine combustion simulations with primary reference fuels;Ra;Combust Flame,2008

4. Enhancement on a skeletal kinetic model for primary reference fuel oxidation by using a semi-decoupling methodology;Liu;Energy Fuels,2012

5. Modeling investigation of different methods to suppress engine knock on a small spark ignition engine;Shao;J Eng Gas Turbines Power,2015

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