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Atomization and Sprays

Published 12 issues per year

ISSN Print: 1044-5110

ISSN Online: 1936-2684

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 1.2 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 1.8 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.3 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00095 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.28 SJR: 0.341 SNIP: 0.536 CiteScore™:: 1.9 H-Index: 57

Indexed in

REVIEW OF ATOMIZATION: CURRENT KNOWLEDGE AND FUTURE REQUIREMENTS FOR PROPULSION COMBUSTORS

Volume 20, Issue 6, 2010, pp. 485-512
DOI: 10.1615/AtomizSpr.v20.i6.20
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ABSTRACT

This paper reviews the current status of understanding, theory, and models for the physics of liquid fuel atomization, particularly as it applies to gas turbine and rocket applications. The paper covers five areas pertinent to atomization issues in gas turbine and rocket combustors: (1) major references in subtopic areas, (2) state-of-the-art understanding of the physical mechanisms in atomization and vaporization for gas turbine and rocket combustors, (3) models and limitations of such models, (4) references to available data sets, and (5) identification of research gaps. Although written specifically to address the requirements for rocket and gas turbine atomization, this paper identifies issues and concerns that are of interest to other users and practitioners of atomization devices, as well as developers of custom and commercial computational fluid dynamics (CFD) codes. Members of the Institute for Liquid Atomization and Spray Systems (ILASS), Americas' Rocket and Air Breathing Power Fuel Atomization Committee, made the bulk of the contributions to this paper. This paper is revised from the version presented by Benjamin and Jensen at the Eighth International Conference on Liquid Atomization and Spray Systems (ICLASS−2000), Pasadena, California, July 16−20, 2000.

CITED BY
  1. Sojka Paul, A Brief History of Advances in our Understanding of Sprays: The Coupled Roles of Measurements and Analyses, 6th AIAA Theoretical Fluid Mechanics Conference, 2011. Crossref

  2. Tharakan T. John, Mukhopadhyay Achintya, Datta Amitava, Jog Milind A., Trends in Comprehensive Modeling of Spray Formation, International Journal of Spray and Combustion Dynamics, 5, 2, 2013. Crossref

  3. Zhao Hui, Liu Hai-Feng, Xu Jian-Liang, Li Wei-Feng, Lin Kuang-Fei, Inhomogeneity in breakup of suspensions, Physics of Fluids, 27, 6, 2015. Crossref

  4. Wang Yifei, Guo Qiangqiang, Yan Liucheng, Zhao Hui, Yu Guangsuo, Wang Fuchen, Research on atomized droplet size in composite quench chamber, The Canadian Journal of Chemical Engineering, 93, 12, 2015. Crossref

  5. Sforzo Brandon A., Kastengren Alan L., Matusik Katarzyna E., Gomez del Campo Felipe, Powell Christopher F., X-Ray Phase Contrast Imaging of Liquid Film and Spray Development Inside an Aircraft Engine Swirler, Journal of Engineering for Gas Turbines and Power, 141, 12, 2019. Crossref

  6. Magnotti Gina M., Lin Kuo-Cheng, Carter Campbell D., Kastengren Alan, Som Sibendu, A Computational Investigation of the Effect of Surface Roughness on the Development of a Liquid Jet in Subsonic Crossflow, AIAA Propulsion and Energy 2020 Forum, 2020. Crossref

  7. Nykteri Georgia, Gavaises Manolis, Droplet aerobreakup under the shear-induced entrainment regime using a multiscale two-fluid approach, Physical Review Fluids, 6, 8, 2021. Crossref

  8. Mohandas Anu, Luo Hongrong, Ramakrishna Seeram, An Overview on Atomization and Its Drug Delivery and Biomedical Applications, Applied Sciences, 11, 11, 2021. Crossref

  9. Zhang Shuai, Gou Wenjin, Wang Yuqi, Zhang Jifa, Zheng Yao, Direct numerical simulation of atomization by jet impact using moving particle semi-implicit method with GPU acceleration, Computational Particle Mechanics, 9, 3, 2022. Crossref

  10. Rossano Viola, Cittadini Amedeo, De Stefano Giuliano, Computational Evaluation of Shock Wave Interaction with a Liquid Droplet, Applied Sciences, 12, 3, 2022. Crossref

  11. Koukouvinis Phoevos, Rodriguez Carlos, Hwang Joonsik, Karathanassis Ioannis, Gavaises Manolis, Pickett Lyle, Machine Learning and transcritical sprays: A demonstration study of their potential in ECN Spray-A, International Journal of Engine Research, 23, 9, 2022. Crossref

  12. Ma Yarui, Cui Jiwen, Tan Jiubin, Quantitative Expression of a Slight Deviation of the Impact Angle in a Collision Atomizer, Machines, 10, 9, 2022. Crossref

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