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A method for the evaluation of damage on the surface of carbon-carbon ablation samplesThe effect of weave geometry on the onset of transition from laminar to turbulent flow around a sample of an orthogonally woven fine weave carbon-carbon material tested in an arc-jet is investigated. Seventeen post-test models which had undergone only partial transition around the circumference were examined as to location of turbulent regions relative to the weave axes. It was statistically shown that the weave axes had the lowest probability of being a position of initial transition onset. The probability generally increased with distance from a major axis, with some rays, notably the 45 deg rays, showing better transition resistance than the adjacent rays. The incidence of initial transition onset correlated well with the number of X or Y fibers that the flow passes over from stagnation point to the shoulder.
Document ID
19760004040
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Heinonen, E. W.
(Air Force Materials Lab. Wright-Patterson AFB, OH, United States)
Jumper, G. Y., Jr.
(Air Force Materials Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-15
Accession Number
76N11128
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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