{"title":"现实旋转起爆发动机中爆炸传播的拉格朗日条件统计","authors":"Caleb Van Beck, Venkat Raman","doi":"10.1016/j.proci.2024.105606","DOIUrl":null,"url":null,"abstract":"Flow behavior was investigated in an RDE using Lagrangian Particle Tracking coupled with high-fidelity Eulerian simulations. The case considered utilized the AFRL Radial Air Inlet design under stoichiometric hydrogen–air conditions at a specified mass flow rate, with a single wave observed in the system. Particle properties were recorded throughout the simulation to compare to Eulerian data as well as to examine the effect of particle injection location on resulting flow behavior. The Lagrangian description of the flow closely resembled the Eulerian description in terms of capturing the detonation wave front properly, but axial velocities between the two descriptions varied significantly due to the moving particles increasing the average recorded velocities within the flow. Injection location was examined based on three conditions, namely starting injection locations 5° ahead of the detonation wave, 5° behind, and 180° ahead. Results showed differing behavior in the 180° condition, wherein a pressure rise was seen further axially into the chamber from detonation wave contact. Particle data was also viewed from a thermodynamic cycle standpoint and compared against an ideal detonative process from a reduced-order cycle deck model. Each injection condition studied failed to fully represent the ideal detonative process, despite showing similar overall trends between enthalpy and entropy, with the highest peak enthalpy coming within 23.75% of the ideal enthalpy in the 180° condition. Heat release behavior aided in understanding deflagrative losses incurred in certain injection conditions. An optimal injection location of 26° ahead of the wave was determined based on maximum pressure rise, which also failed to produce fully ideal thermodynamic behavior. Overall, this analysis shows the value of examining RDE flow from a Lagrangian perspective, given the insight it yields into how fluid interacts with flow structures inside complex RDE systems and how this translates to thermodynamic space for comparison to ideal behavior.","PeriodicalId":408,"journal":{"name":"Proceedings of the Combustion Institute","volume":"31 1","pages":""},"PeriodicalIF":5.3000,"publicationDate":"2024-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Lagrangian-conditioned statistics of detonation propagation in a realistic rotating detonation engine\",\"authors\":\"Caleb Van Beck, Venkat Raman\",\"doi\":\"10.1016/j.proci.2024.105606\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Flow behavior was investigated in an RDE using Lagrangian Particle Tracking coupled with high-fidelity Eulerian simulations. The case considered utilized the AFRL Radial Air Inlet design under stoichiometric hydrogen–air conditions at a specified mass flow rate, with a single wave observed in the system. Particle properties were recorded throughout the simulation to compare to Eulerian data as well as to examine the effect of particle injection location on resulting flow behavior. The Lagrangian description of the flow closely resembled the Eulerian description in terms of capturing the detonation wave front properly, but axial velocities between the two descriptions varied significantly due to the moving particles increasing the average recorded velocities within the flow. Injection location was examined based on three conditions, namely starting injection locations 5° ahead of the detonation wave, 5° behind, and 180° ahead. Results showed differing behavior in the 180° condition, wherein a pressure rise was seen further axially into the chamber from detonation wave contact. Particle data was also viewed from a thermodynamic cycle standpoint and compared against an ideal detonative process from a reduced-order cycle deck model. Each injection condition studied failed to fully represent the ideal detonative process, despite showing similar overall trends between enthalpy and entropy, with the highest peak enthalpy coming within 23.75% of the ideal enthalpy in the 180° condition. Heat release behavior aided in understanding deflagrative losses incurred in certain injection conditions. An optimal injection location of 26° ahead of the wave was determined based on maximum pressure rise, which also failed to produce fully ideal thermodynamic behavior. Overall, this analysis shows the value of examining RDE flow from a Lagrangian perspective, given the insight it yields into how fluid interacts with flow structures inside complex RDE systems and how this translates to thermodynamic space for comparison to ideal behavior.\",\"PeriodicalId\":408,\"journal\":{\"name\":\"Proceedings of the Combustion Institute\",\"volume\":\"31 1\",\"pages\":\"\"},\"PeriodicalIF\":5.3000,\"publicationDate\":\"2024-09-02\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the Combustion Institute\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.1016/j.proci.2024.105606\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENERGY & FUELS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Combustion Institute","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1016/j.proci.2024.105606","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
Lagrangian-conditioned statistics of detonation propagation in a realistic rotating detonation engine
Flow behavior was investigated in an RDE using Lagrangian Particle Tracking coupled with high-fidelity Eulerian simulations. The case considered utilized the AFRL Radial Air Inlet design under stoichiometric hydrogen–air conditions at a specified mass flow rate, with a single wave observed in the system. Particle properties were recorded throughout the simulation to compare to Eulerian data as well as to examine the effect of particle injection location on resulting flow behavior. The Lagrangian description of the flow closely resembled the Eulerian description in terms of capturing the detonation wave front properly, but axial velocities between the two descriptions varied significantly due to the moving particles increasing the average recorded velocities within the flow. Injection location was examined based on three conditions, namely starting injection locations 5° ahead of the detonation wave, 5° behind, and 180° ahead. Results showed differing behavior in the 180° condition, wherein a pressure rise was seen further axially into the chamber from detonation wave contact. Particle data was also viewed from a thermodynamic cycle standpoint and compared against an ideal detonative process from a reduced-order cycle deck model. Each injection condition studied failed to fully represent the ideal detonative process, despite showing similar overall trends between enthalpy and entropy, with the highest peak enthalpy coming within 23.75% of the ideal enthalpy in the 180° condition. Heat release behavior aided in understanding deflagrative losses incurred in certain injection conditions. An optimal injection location of 26° ahead of the wave was determined based on maximum pressure rise, which also failed to produce fully ideal thermodynamic behavior. Overall, this analysis shows the value of examining RDE flow from a Lagrangian perspective, given the insight it yields into how fluid interacts with flow structures inside complex RDE systems and how this translates to thermodynamic space for comparison to ideal behavior.
期刊介绍:
The Proceedings of the Combustion Institute contains forefront contributions in fundamentals and applications of combustion science. For more than 50 years, the Combustion Institute has served as the peak international society for dissemination of scientific and technical research in the combustion field. In addition to author submissions, the Proceedings of the Combustion Institute includes the Institute''s prestigious invited strategic and topical reviews that represent indispensable resources for emergent research in the field. All papers are subjected to rigorous peer review.
Research papers and invited topical reviews; Reaction Kinetics; Soot, PAH, and other large molecules; Diagnostics; Laminar Flames; Turbulent Flames; Heterogeneous Combustion; Spray and Droplet Combustion; Detonations, Explosions & Supersonic Combustion; Fire Research; Stationary Combustion Systems; IC Engine and Gas Turbine Combustion; New Technology Concepts
The electronic version of Proceedings of the Combustion Institute contains supplemental material such as reaction mechanisms, illustrating movies, and other data.