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Magnetohydrodynamics Accelerator Research into Advanced Hypersonics (MARIAH)This report documents the activities, results, conclusions and recommendations of the Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (MARIAH) Project in which the use of magnetohydrodynamics (MHD) technology is investigated for its applicability to augment hypersonic wind tunnels. The long range objective of this investigation is to advance the development of ground test facilities to support the development of hypervelocity flight vehicles. The MHD accelerator adds kinetic energy directly to the wind tunnel working fluid, thereby increasing its Mach number to hypervelocity levels. Several techniques for MHD augmentation, as well as other physical characteristics of the process are studied to enhance the overall performance of hypersonic wind tunnel design. Specific recommendations are presented to improve the effectiveness of ground test facilities. The work contained herein builds on nearly four decades of research and experimentation by the aeronautics ground test and evaluation community, both foreign and domestic.
Document ID
19980000959
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Baughman, Jack A.
(MSE Technology Applications, Inc. Butte, MT United States)
Micheletti, David A.
(MSE Technology Applications, Inc. Butte, MT United States)
Nelson, Gordon L.
(MSE Technology Applications, Inc. Butte, MT United States)
Simmons, Gloyd A.
(MSE Technology Applications, Inc. Butte, MT United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1997
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
MSE-029-Pt-2
NASA/CR-97-206242-Pt-2
NAS 1.26:206242-Pt-2
Report Number: MSE-029-Pt-2
Report Number: NASA/CR-97-206242-Pt-2
Report Number: NAS 1.26:206242-Pt-2
Funding Number(s)
CONTRACT_GRANT: NASA Order A-45416-D
CONTRACT_GRANT: DE-AC22-96EW-96405
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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