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Effect of Plasma Sheaths on Earth Re-entry MHD ProcessesThe first study of the full coupling between the aerothermodynamics, the magnetohydrodynamics, and the plasma sheaths within earth entry flows is here per-formed. The problem tackled herein is representative of a force-generating MHD patch located between the plenum and the frustum of a capsule entering the earth’s atmosphere at Mach 34. The reactions are obtained from a modified 11-species Park chemical solver. The physical model fully couples the drift-diffusion model for the sheaths to the multispecies Navier-Stokes equations for the plasma flow. The Hall and ion slip effects are taken into consideration within the plasma flow and within the sheaths. Results obtained indicate that the cathode sheath can exert significant resistance to current flow and thus reduce the MHD-generated force by 40% or more. The effect of the sheath on the MHD force is found to be more pronounced at lower applied magnetic field.
Document ID
20210016754
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Bernard Parent
(University of Arizona Tucson, Arizona, United States)
Prasanna T. Rajendran
(University of Arizona Tucson, Arizona, United States)
Robert W Moses
(Langley Research Center Hampton, Virginia, United States)
Christopher O Johnston
(Langley Research Center Hampton, Virginia, United States)
F Mcneil Cheatwood
(Langley Research Center Hampton, Virginia, United States)
Sergey O Macheret
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Justin Little
(University of Washington Seattle, WA)
Date Acquired
June 1, 2021
Subject Category
Plasma Physics
Meeting Information
Meeting: AIAA SciTech 2022
Location: San Deigo, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80NSSC20K1836
Distribution Limits
Public
Copyright
Public Use Permitted.
Patent
This NTR was assigned LAR-2033-1 - which was indicated as Do Not Patent in June 2021
Patent Application
Keywords
Earth Re-entry
magnetohydrodynamics
MHD modeling
aerothermodynamics
aerocapture
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