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International Journal of Energetic Materials and Chemical Propulsion

Publication de 6  numéros par an

ISSN Imprimer: 2150-766X

ISSN En ligne: 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

Indexed in

COMPARISON OF PIV AND COLOUR-SCHLIEREN MEASUREMENTS OF THE COMBUSTION PROCESS OF BORON PARTICLE CONTAINING SOLID FUEL SLABS IN A REARWARD FACING STEP COMBUSTOR

Volume 5, Numéro 1-6, 2002, pp. 742-752
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.770
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RÉSUMÉ

Particle Image Velocimetry (PIV) and Colour-Schlieren measurements have been used in order to investigate the combustion process of solid fuel slabs with boron particle addition in a step combustor under ramjet relevant conditions concerning the air inlet temperature. The high time-resolution of both measurement techniques (∼13 μs for Schlieren and 10 ns for PIV) shows a quasi-frozen state of the flow. With both techniques, large-scale vortical structures were observed in the outer zone above the diffusion flame in the developing boundary layer behind the recirculation zone.

CITÉ PAR
  1. Petrarolo Anna, Kobald Mario, Schlechtriem Stefan, Visualization of Combustion Phenomena in Paraffin-Based Hybrid Rocket Fuels at Super-Critical Pressures, 2018 Joint Propulsion Conference, 2018. Crossref

  2. Kobald Mario, Petrarolo Anna, Schlechtriem Stefan, Combustion Visualization and Characterization of Liquefying Hybrid Rocket Fuels, 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015. Crossref

  3. Kobald Mario, Verri Isabella, Schlechtriem Stefan, Theoretical and experimental analysis of liquid layer instability in hybrid rocket engines, CEAS Space Journal, 7, 1, 2015. Crossref

  4. Rüttgers A., Petrarolo A., Kobald M., Clustering of paraffin-based hybrid rocket fuels combustion data, Experiments in Fluids, 61, 1, 2020. Crossref

  5. Kobald Mario, Ciezki Helmut, Schlechtriem Stefan, Optical Investigation of the Combustion Process in Paraffin-based Hybrid Rocket Fuels, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013. Crossref

  6. Petrarolo Anna, Ruettgers Alexander, Kobald Mario, Data Clustering of Hybrid Rocket Combustion Flame, AIAA Propulsion and Energy 2019 Forum, 2019. Crossref

  7. Rüttgers A.,  Petrarolo A., Local anomaly detection in hybrid rocket combustion tests, Experiments in Fluids, 62, 7, 2021. Crossref

  8. Veraar Ronald G., Oosthuisen R. , Andersson K. , RAMJET PROPULSION FOR PROJECTILES-AN OVERVIEW OF WORLDWIDE ACHIEVEMENTS AND FUTURE OPPORTUNITIES , International Journal of Energetic Materials and Chemical Propulsion, 21, 5, 2022. Crossref

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