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Initial investigation of cryogenic wind tunnel model filler materialsVarious filler materials are being investigated for applicability to cryogenic wind tunnel models. The filler materials will be used to fill surface grooves, holes and flaws. The severe test environment of cryogenic models precludes usage of filler materials used on conventional wind tunnel models. Coefficients of thermal expansion, finishing characteristics, adhesion and stability of several candidate filler materials were examined. Promising filler materials are identified.
Document ID
19850009760
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rush, H. F.
(NASA Langley Research Center Hampton, VA, United States)
Firth, G. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:86363
NASA-TM-86363
Accession Number
85N18069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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