Analytical model for electrohydrodynamic thrust

Author:

Vaddi Ravi Sankar1ORCID,Guan Yifei2ORCID,Mamishev Alexander3,Novosselov Igor14ORCID

Affiliation:

1. Department of Mechanical Engineering, University of Washington, Seattle, WA, USA

2. Department of Mechanical Engineering, Rice University, Houston, TX, USA

3. Department of Electrical and Computer Engineering, University of Washington, Seattle, WA, USA

4. Institute of Nano-Engineering Sciences, University of Washington, Seattle, WA, USA

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.

Funder

Intelligence Advanced Research Projects Activity

Joint Center for Aerospace Technology Innovation

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Reference44 articles.

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