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Jet engine powers large, high-temperature wind tunnelWind tunnel for large component testing uses a jet engine with afterburner to provide high temperatures /1200 degrees to 2000 degrees F/ and controlled high velocity gas. This economical wind tunnel can accommodate parts ten feet by ten feet or larger, and is a useful technique for qualitative information.
Document ID
19670000620
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Benham, T. F.
Mulliken, S. R.
Date Acquired
August 3, 2013
Publication Date
December 1, 1967
Subject Category
Physical Sciences
Report/Patent Number
MFS-13544
Accession Number
67B10621
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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