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Experimental investigation of auto-ignition of ethylene-nitrous oxide propellants in rapid compression machine
•Rapid compression machine experiments.•Ethylene-nitrous oxide propellants.•Ignition delay times at low-T regime.•Chemical kinetic model of N2O-C2H4. Considering the available experimental investigations of auto-ignition behaviors of N2O-C2 hydrocarbons propellants are limited in high-temperature re...
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Published in: | Fuel (Guildford) 2021-03, Vol.288, p.119688, Article 119688 |
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creator | Zhang, Feng Chen, Hong-yu Feng, Jian-chang Zheng, Dong |
description | •Rapid compression machine experiments.•Ethylene-nitrous oxide propellants.•Ignition delay times at low-T regime.•Chemical kinetic model of N2O-C2H4.
Considering the available experimental investigations of auto-ignition behaviors of N2O-C2 hydrocarbons propellants are limited in high-temperature regime, in the work the ignition delay times for N2O-C2H4 propellants have been measured under the conditions of TC = 885–940 K, PC = 2.5–4.3 MPa, φ = 1.05 and 1.35 using the rapid compression machine experiments. Then the relational expression between ignition delay time and condition factors is derived as lgτig=11.781000/Tc-0.26Pc-0.83φ-9.41 by linear fitting. The expression can be used to predict ignition delay times of N2O-C2H4 propellants in practice. Moreover, the calculated ignition delay times by three kinetic models are compared with experimental data. The results show that these models can well predict ignition behaviors at high temperature regime, but fail at low-temperature regime. Through temperature sensitivity analysis, at high-temperature regime the N2O decomposition reaction has the highest sensitivity coefficient and dominated the overall reaction. While at low-temperature regime, the oxidation reactions of N2O and hydrocarbons become more important steps. For better prediction of low-temperature ignition behaviors, the low-temperature oxidation mechanism of N2O and hydrocarbons needs further development, and the kinetic parameters of the highly sensitive reactions should be improved. |
doi_str_mv | 10.1016/j.fuel.2020.119688 |
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Considering the available experimental investigations of auto-ignition behaviors of N2O-C2 hydrocarbons propellants are limited in high-temperature regime, in the work the ignition delay times for N2O-C2H4 propellants have been measured under the conditions of TC = 885–940 K, PC = 2.5–4.3 MPa, φ = 1.05 and 1.35 using the rapid compression machine experiments. Then the relational expression between ignition delay time and condition factors is derived as lgτig=11.781000/Tc-0.26Pc-0.83φ-9.41 by linear fitting. The expression can be used to predict ignition delay times of N2O-C2H4 propellants in practice. Moreover, the calculated ignition delay times by three kinetic models are compared with experimental data. The results show that these models can well predict ignition behaviors at high temperature regime, but fail at low-temperature regime. Through temperature sensitivity analysis, at high-temperature regime the N2O decomposition reaction has the highest sensitivity coefficient and dominated the overall reaction. While at low-temperature regime, the oxidation reactions of N2O and hydrocarbons become more important steps. For better prediction of low-temperature ignition behaviors, the low-temperature oxidation mechanism of N2O and hydrocarbons needs further development, and the kinetic parameters of the highly sensitive reactions should be improved.</description><identifier>ISSN: 0016-2361</identifier><identifier>EISSN: 1873-7153</identifier><identifier>DOI: 10.1016/j.fuel.2020.119688</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>Auto-ignition ; Compression ; Decomposition reactions ; Delay time ; Ethylene ; High temperature ; Hydrocarbons ; Ignition ; Ignition delay time ; Low temperature ; Nitrous oxide ; Oxidation ; Parameter sensitivity ; Propellants ; Rapid compression machine ; Sensitivity analysis ; Spontaneous combustion ; Temperature</subject><ispartof>Fuel (Guildford), 2021-03, Vol.288, p.119688, Article 119688</ispartof><rights>2020 Elsevier Ltd</rights><rights>Copyright Elsevier BV Mar 15, 2021</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c328t-5cc06408df5387c1a18d15b732d50abb6327a0aaaf8f4e832cc94561ceb8f72b3</citedby><cites>FETCH-LOGICAL-c328t-5cc06408df5387c1a18d15b732d50abb6327a0aaaf8f4e832cc94561ceb8f72b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Zhang, Feng</creatorcontrib><creatorcontrib>Chen, Hong-yu</creatorcontrib><creatorcontrib>Feng, Jian-chang</creatorcontrib><creatorcontrib>Zheng, Dong</creatorcontrib><title>Experimental investigation of auto-ignition of ethylene-nitrous oxide propellants in rapid compression machine</title><title>Fuel (Guildford)</title><description>•Rapid compression machine experiments.•Ethylene-nitrous oxide propellants.•Ignition delay times at low-T regime.•Chemical kinetic model of N2O-C2H4.
Considering the available experimental investigations of auto-ignition behaviors of N2O-C2 hydrocarbons propellants are limited in high-temperature regime, in the work the ignition delay times for N2O-C2H4 propellants have been measured under the conditions of TC = 885–940 K, PC = 2.5–4.3 MPa, φ = 1.05 and 1.35 using the rapid compression machine experiments. Then the relational expression between ignition delay time and condition factors is derived as lgτig=11.781000/Tc-0.26Pc-0.83φ-9.41 by linear fitting. The expression can be used to predict ignition delay times of N2O-C2H4 propellants in practice. Moreover, the calculated ignition delay times by three kinetic models are compared with experimental data. The results show that these models can well predict ignition behaviors at high temperature regime, but fail at low-temperature regime. Through temperature sensitivity analysis, at high-temperature regime the N2O decomposition reaction has the highest sensitivity coefficient and dominated the overall reaction. While at low-temperature regime, the oxidation reactions of N2O and hydrocarbons become more important steps. For better prediction of low-temperature ignition behaviors, the low-temperature oxidation mechanism of N2O and hydrocarbons needs further development, and the kinetic parameters of the highly sensitive reactions should be improved.</description><subject>Auto-ignition</subject><subject>Compression</subject><subject>Decomposition reactions</subject><subject>Delay time</subject><subject>Ethylene</subject><subject>High temperature</subject><subject>Hydrocarbons</subject><subject>Ignition</subject><subject>Ignition delay time</subject><subject>Low temperature</subject><subject>Nitrous oxide</subject><subject>Oxidation</subject><subject>Parameter sensitivity</subject><subject>Propellants</subject><subject>Rapid compression machine</subject><subject>Sensitivity analysis</subject><subject>Spontaneous combustion</subject><subject>Temperature</subject><issn>0016-2361</issn><issn>1873-7153</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kEtPwzAQhC0EEqXwBzhF4pziR5y4EhdUlYdUiQucLcfZtK5SO9hO1f57HAWunFYazczufgjdE7wgmJSP-0U7QLegmCaBLEshLtCMiIrlFeHsEs1wcuWUleQa3YSwxxhXghczZNenHrw5gI2qy4w9Qohmq6JxNnNtpobocrO15k-AuDt3YCFPkndDyNzJNJD13vXQdcrGkEoyr3rTZNodeg8hjNGD0jtj4RZdtaoLcPc75-jrZf25ess3H6_vq-dNrhkVMeda47LAomk5E5UmioiG8LpitOFY1XXJaKWwUqoVbQGCUa2XBS-Jhlq0Fa3ZHD1Mvemw7yH9JPdu8DatlLQQS0wZxyS56OTS3oXgoZV9QqH8WRIsR65yL0eucuQqJ64p9DSFIN1_NOBl0AashsZ40FE2zvwX_wH9oIQB</recordid><startdate>20210315</startdate><enddate>20210315</enddate><creator>Zhang, Feng</creator><creator>Chen, Hong-yu</creator><creator>Feng, Jian-chang</creator><creator>Zheng, Dong</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7QO</scope><scope>7QQ</scope><scope>7SC</scope><scope>7SE</scope><scope>7SP</scope><scope>7SR</scope><scope>7T7</scope><scope>7TA</scope><scope>7TB</scope><scope>7U5</scope><scope>8BQ</scope><scope>8FD</scope><scope>C1K</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>H8G</scope><scope>JG9</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>P64</scope></search><sort><creationdate>20210315</creationdate><title>Experimental investigation of auto-ignition of ethylene-nitrous oxide propellants in rapid compression machine</title><author>Zhang, Feng ; Chen, Hong-yu ; Feng, Jian-chang ; Zheng, Dong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c328t-5cc06408df5387c1a18d15b732d50abb6327a0aaaf8f4e832cc94561ceb8f72b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Auto-ignition</topic><topic>Compression</topic><topic>Decomposition reactions</topic><topic>Delay time</topic><topic>Ethylene</topic><topic>High temperature</topic><topic>Hydrocarbons</topic><topic>Ignition</topic><topic>Ignition delay time</topic><topic>Low temperature</topic><topic>Nitrous oxide</topic><topic>Oxidation</topic><topic>Parameter sensitivity</topic><topic>Propellants</topic><topic>Rapid compression machine</topic><topic>Sensitivity analysis</topic><topic>Spontaneous combustion</topic><topic>Temperature</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Feng</creatorcontrib><creatorcontrib>Chen, Hong-yu</creatorcontrib><creatorcontrib>Feng, Jian-chang</creatorcontrib><creatorcontrib>Zheng, Dong</creatorcontrib><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Biotechnology Research Abstracts</collection><collection>Ceramic Abstracts</collection><collection>Computer and Information Systems Abstracts</collection><collection>Corrosion Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Industrial and Applied Microbiology Abstracts (Microbiology A)</collection><collection>Materials Business File</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Copper Technical Reference Library</collection><collection>Materials Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>Biotechnology and BioEngineering Abstracts</collection><jtitle>Fuel (Guildford)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Feng</au><au>Chen, Hong-yu</au><au>Feng, Jian-chang</au><au>Zheng, Dong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental investigation of auto-ignition of ethylene-nitrous oxide propellants in rapid compression machine</atitle><jtitle>Fuel (Guildford)</jtitle><date>2021-03-15</date><risdate>2021</risdate><volume>288</volume><spage>119688</spage><pages>119688-</pages><artnum>119688</artnum><issn>0016-2361</issn><eissn>1873-7153</eissn><abstract>•Rapid compression machine experiments.•Ethylene-nitrous oxide propellants.•Ignition delay times at low-T regime.•Chemical kinetic model of N2O-C2H4.
Considering the available experimental investigations of auto-ignition behaviors of N2O-C2 hydrocarbons propellants are limited in high-temperature regime, in the work the ignition delay times for N2O-C2H4 propellants have been measured under the conditions of TC = 885–940 K, PC = 2.5–4.3 MPa, φ = 1.05 and 1.35 using the rapid compression machine experiments. Then the relational expression between ignition delay time and condition factors is derived as lgτig=11.781000/Tc-0.26Pc-0.83φ-9.41 by linear fitting. The expression can be used to predict ignition delay times of N2O-C2H4 propellants in practice. Moreover, the calculated ignition delay times by three kinetic models are compared with experimental data. The results show that these models can well predict ignition behaviors at high temperature regime, but fail at low-temperature regime. Through temperature sensitivity analysis, at high-temperature regime the N2O decomposition reaction has the highest sensitivity coefficient and dominated the overall reaction. While at low-temperature regime, the oxidation reactions of N2O and hydrocarbons become more important steps. For better prediction of low-temperature ignition behaviors, the low-temperature oxidation mechanism of N2O and hydrocarbons needs further development, and the kinetic parameters of the highly sensitive reactions should be improved.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.fuel.2020.119688</doi></addata></record> |
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subjects | Auto-ignition Compression Decomposition reactions Delay time Ethylene High temperature Hydrocarbons Ignition Ignition delay time Low temperature Nitrous oxide Oxidation Parameter sensitivity Propellants Rapid compression machine Sensitivity analysis Spontaneous combustion Temperature |
title | Experimental investigation of auto-ignition of ethylene-nitrous oxide propellants in rapid compression machine |
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