The hyperthermal supersonic aerodynamic tunnel.Electric-arc-heated hyperthermal wind tunnel operation and improvement by enthalpy output increase and optimal use at tunnel throat
Document ID
19650033496
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stine, H. A.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-RP-360Report Number: NASA-RP-360
Accession Number
65A16200
Distribution Limits
Public
Copyright
Other
Keywords
WIND TUNNELARC HEATING
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Related Records
IDRelationTitle19650033492Collected WorksHigh temperature technology, international union of pure and applied chemistry, commission on high temperatures and refractories, international symposium, pacific grove, calif., september 8-11, 1963, proceedings.19650033492Collected WorksHigh temperature technology, international union of pure and applied chemistry, commission on high temperatures and refractories, international symposium, pacific grove, calif., september 8-11, 1963, proceedings.