Analytical model for electrohydrodynamic thrust

Abstract

Electrohydrodynamic (EHD) thrust is produced when ionized fluid is accelerated in an electric field due to the momentum transfer between the charged species and neutral molecules. We extend the previously reported analytical model that couples space charge, electric field and momentum transfer to derive thrust force in one-dimensional planar coordinates. The electric current density in the model can be expressed in the form of Mott–Gurney law. After the correction for the drag force, the EHD thrust model yields good agreement with the experimental data from several independent studies. The EHD thrust expression derived from the first principles can be used in the design of propulsion systems and can be readily implemented in the numerical simulations.

Document Details

Document Type
Pub Defense Publication
Publication Date
Sep 01, 2020
Source ID
10.1098/rspa.2020.0220

Entities

People

  • Alexander Mamishev
  • Igor Novosselov
  • Ravi Sankar Vaddi
  • Yifei Guan

Organizations

  • Intelligence Advanced Research Projects Activity
  • Rice University
  • University of Washington

Tags

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster