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International Journal of Energetic Materials and Chemical Propulsion

Erscheint 6 Ausgaben pro Jahr

ISSN Druckformat: 2150-766X

ISSN Online: 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

SCIENCE-BASED SIMULATION TOOLS FOR HAZARD ASSESSMENT AND MITIGATION

Volumen 8, Ausgabe 5, 2009, pp. 373-389
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v8.i5.10
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ABSTRAKT

Solid rocket motors consist of hollow cylindrical grains of energetic solid propellant that are designed to be ignited in the bore and burn from the inside out. However, many common rocket motor accident scenarios involve mechanical or thermal insults to the outside case of the rocket. This can lead to ignition at the interface of the propellant and liner (i.e., outside-in combustion), and a resulting explosion. In this paper, we describe a state-of-the-art high-performance simulation program that can be used to predict the violence of explosions and aid the design of devices to mitigate the violence of accidental explosions during transportation and storage.

REFERENZEN
  1. de St. Germain, J.D., McCorquodale, J., Parker, S.G., and Johnson, C.R., Uintah, A Massively Parallel Problem Solving Environment.

  2. Guilkey, J., Harman, T., and Banerjee, B., An Eulerian-Lagrangian Approach for Simulating Explosions of Energetic Devices.

  3. Ward, M.J., Son, S.F., and Brewster, M.Q., Steady Deflagration of HMX with Simple Kinetics, A Gas Phase Chain Reaction Model.

  4. Ward, M.J., Son, S.F., and Brewster, M.Q., Role of Gas- and Condensed-Phase Kinetics in Burning Rate Control of Energetic Solids.

  5. Atwood, A.I., Boggs, T.L., Curran, P.O., Parr, T.P., Hanson-Parr, D.M., Price, C.F., and Wiknich, J., Burning Rate of Solid Propellant Ingredients, Part 1, Pressure and Initial Temperature Effects.

  6. Finlinson, J.C., Stalnaker, R., and Blomshield, F.S., HMX and RDX T-Burner Pressure Coupled Response from 200 to 1000 psi.

  7. Finlinson, J.C., Stalnaker, R., and Blomshield, F.S., HMX T-Burner Pressure Coupled Response at 200, 500, and 1000 psi.

  8. Finlinson, J.C. and Stalnaker, R., Pure Oxidizer T-Burner Pressure Coupled Response For AP, HMX, RDX From 200 to 1000 psi.

  9. Eddings, E.G., Ciro, W., and Wight, C.A., High Energy Materials in Fires, Influence of Fire Environment on Violence of Reactions.

  10. Eddings, E.G., Ciro, W., and Sarofim, A.F., Transient Heat Transfer in Exploding and Detonating Systems.

  11. Beck, J.V., Blackwell, B., and Clair, C.S., Inverse Heat Conduction, Ill-Posed Problems.

  12. Beckstead, M., An Ignition Model for Modern Double Base Propellants.

REFERENZIERT VON
  1. Beckvermit Jacqueline, Harman Todd, Wight Charles, Berzins Martin, Packing Configurations of PBX‐9501 Cylinders to Reduce the Probability of a Deflagration to Detonation Transition (DDT), Propellants, Explosives, Pyrotechnics, 41, 6, 2016. Crossref

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