Deborah Levin Fliflet

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Research Output

A Self-Consistent Open Boundary Condition for Fully Kinetic Plasma Thruster Plume Simulations

Jambunathan, R. & Levin, D. A., Mar 2020, In : IEEE Transactions on Plasma Science. 48, 3, p. 610-630 21 p., 8986756.

Research output: Contribution to journalArticle

  • 3D detailed far field plume modeling of SPT-100

    Tekinalp, A. & Levin, D. A., Jan 1 2019, AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Propulsion and Energy Forum and Exposition, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • Electrospray molecular dynamics simulations using an octree-based Coulomb interaction method

    Mehta, N. A. & Levin, D. A., Mar 11 2019, In : Physical Review E. 99, 3, 033302.

    Research output: Contribution to journalArticle

  • Kinetic modeling of parasitic currents on spacecraft surfaces due to ambient space plasmas

    Nuwal, N. & Levin, D. A., Jan 1 2019, AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Propulsion and Energy Forum and Exposition, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution