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International Journal of Energetic Materials and Chemical Propulsion

年間 6 号発行

ISSN 印刷: 2150-766X

ISSN オンライン: 2150-7678

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: 0.7 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: 0.7 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: 0.1 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: 0.00016 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: 0.18 SJR: 0.313 SNIP: 0.6 CiteScore™:: 1.6 H-Index: 16

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ANALYSIS OF QUASI-STEADY AND TRANSIENT BURNING OF HYBRID FUELS IN A LABORATORY-SCALE BURNER BY AN OPTICAL TECHNIQUE

巻 12, 発行 5, 2013, pp. 385-410
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2013005756
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要約

Burning of hydroxyl-terminated polybutadiene in gaseous oxygen is investigated using a time-resolved optical technique. Combustion tests are performed in a two-dimensional radial micro-burner under quasi-steady and forced transient operating conditions. Under quasi-steady operating conditions, the high initial regression rate at the beginning of the run is followed by a smooth monotonic decrease as combustion proceeds. This behavior is captured by a purposely developed regression rate simulation model. Under forced transient operating conditions, for oxidizer mass flow throttling down, solid fuel exhibits a non-monotonic regression rate response. Earlier phases of the transient are characterized by a noticeable regression rate decrease followed by faint oscillations.

によって引用された
  1. De Luca Luigi T., Galfetti Luciano, Maggi Filippo, Colombo Giovanni, Paravan Christian, Reina Alice, Dossi Stefano, Fassina Marco, Sossi Andrea, Characterization and Combustion of Aluminum Nanopowders in Energetic Systems, in Metal Nanopowders, 2014. Crossref

  2. Dossi Stefano, Paravan Christian, Maggi Filippo, Galfetti Luciano, Enhancing Micrometric Aluminum Reactivity by Mechanical Activation, 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015. Crossref

  3. Dossi Stefano, Paravan Christian, Maggi Filippo, Di Lorenzo Marco, Ardalic Jovan, Galfetti Luciano, Novel Activated Metal Powders for Improved Hybrid Fuels and Green Solid Propellants, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. Crossref

  4. Paravan Christian, Galfetti Luciano, Maggi Filippo, A Critical Analysis of Paraffin-based Fuel Formulations for Hybrid Rocket Propulsion, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. Crossref

  5. Paravan Christian, Bisin Riccardo, Lisi Francesco, Galfetti Luciano, Massimo Pietro, Burning Behavior Investigation of a Vortex Flow Pancake Hybrid Rocket Engine, AIAA Propulsion and Energy 2019 Forum, 2019. Crossref

  6. Paravan , Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion, Aerospace, 6, 12, 2019. Crossref

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