{"title":"Performance Enhancement of EAD Thrusters With Nonuniform Emitters Array","authors":"Davide Usuelli;Raffaello Terenzi;Stefano Trovato;Marco Belan","doi":"10.1109/TPS.2024.3505980","DOIUrl":null,"url":null,"abstract":"This work presents an experimental campaign to optimize the performance of electro-aerodynamic (EAD) thrusters through nonuniform emitter arrangements. The study examines the impact of emitter configurations on thrust and thrust-to-power coefficients <inline-formula> <tex-math>$\\boldsymbol {C}_{\\boldsymbol {T}}$ </tex-math></inline-formula> and <inline-formula> <tex-math>$\\boldsymbol {C}_{\\boldsymbol {TP}}$ </tex-math></inline-formula>. Different emitter arrangements, including collinear and staggered arrays, are tested using thrust, electrical, and velocity measurements as diagnostics. The tests are parametrically performed for different sizes (chords) of the collector electrodes. Results reveal that nonuniform emitter configurations outperform standard arrays, in particular, with short chord collectors, widely spaced apart. An optimal configuration for <inline-formula> <tex-math>$\\boldsymbol {C}_{\\boldsymbol {T}}$ </tex-math></inline-formula> is identified among the staggered ones. In addition, droplet collectors demonstrate competitive performance compared to airfoil collectors.","PeriodicalId":450,"journal":{"name":"IEEE Transactions on Plasma Science","volume":"52 11","pages":"5414-5421"},"PeriodicalIF":1.3000,"publicationDate":"2024-12-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=10785549","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Plasma Science","FirstCategoryId":"101","ListUrlMain":"https://ieeexplore.ieee.org/document/10785549/","RegionNum":4,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"PHYSICS, FLUIDS & PLASMAS","Score":null,"Total":0}
引用次数: 0
Abstract
This work presents an experimental campaign to optimize the performance of electro-aerodynamic (EAD) thrusters through nonuniform emitter arrangements. The study examines the impact of emitter configurations on thrust and thrust-to-power coefficients $\boldsymbol {C}_{\boldsymbol {T}}$ and $\boldsymbol {C}_{\boldsymbol {TP}}$ . Different emitter arrangements, including collinear and staggered arrays, are tested using thrust, electrical, and velocity measurements as diagnostics. The tests are parametrically performed for different sizes (chords) of the collector electrodes. Results reveal that nonuniform emitter configurations outperform standard arrays, in particular, with short chord collectors, widely spaced apart. An optimal configuration for $\boldsymbol {C}_{\boldsymbol {T}}$ is identified among the staggered ones. In addition, droplet collectors demonstrate competitive performance compared to airfoil collectors.
期刊介绍:
The scope covers all aspects of the theory and application of plasma science. It includes the following areas: magnetohydrodynamics; thermionics and plasma diodes; basic plasma phenomena; gaseous electronics; microwave/plasma interaction; electron, ion, and plasma sources; space plasmas; intense electron and ion beams; laser-plasma interactions; plasma diagnostics; plasma chemistry and processing; solid-state plasmas; plasma heating; plasma for controlled fusion research; high energy density plasmas; industrial/commercial applications of plasma physics; plasma waves and instabilities; and high power microwave and submillimeter wave generation.