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Problems in J times B plasma acceleration Semiannual progress reportShock tube accelerator, heat transfer gauge, homopolar accelerator theory, and transport effects in boundary layers in plasmas
Document ID
19660006687
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fay, J. A. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Physics, Plasma
Report/Patent Number
NASA-CR-69659
Report Number: NASA-CR-69659
Accession Number
66N15976
Funding Number(s)
CONTRACT_GRANT: NGR-22-009-052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER
HEAT TRANSFER
SHOCK TUNNEL
ACCELERATOR

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