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Cost effective use of liquid nitrogen in cryogenic wind tunnelsA method of reliquefying from 12 to 19% of the nitrogen exhaust gas from a cryogenic wind tunnel has been developed. Technical feasibility and cost effectiveness of the system depends on performance of an innovative positive displacement expander which requires scale model testing to confirm design studies. The existing cryogenic system at the 0.3-m transonic cryogenic tunnel has been surveyed and extensive upgrades proposed. Upgrades are generally cost effective and may be implemented immediately since they are based on established technology.
Document ID
19870014230
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcintosh, Glen E.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Lombard, David S.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Martindale, David L.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Dunn, Robert P.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-178279
NAS 1.26:178279
Report Number: NASA-CR-178279
Report Number: NAS 1.26:178279
Accession Number
87N23663
Funding Number(s)
PROJECT: RTOP 505-61-01-02
CONTRACT_GRANT: NAS1-18216
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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