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Graphite oxidation at low temperature in subsonic air.Coupled mass loss and heat transfer was studied experimentally for thin two inch diameter graphite disks heated as high as 2800 F in a flow of ambient air at velocities of 97 to 717 ft/sec. Oxidation was predominately reaction rate controlled with rate constants which were determined experimentally for POCO AXF 5Q, ATJ, ATJS, and an AVCO 3D Orthogonal material. The specimen thermal response was used with an energy balance to obtain the influence of mass loss and chemical reactions on the heat transfer. Specimen heating due to exothermic reactions correlates qualitatively with an approximate theory.
Document ID
19730051550
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Knight, D. D.
(General Electric Co. Valley Forge, Pa., United States)
Knechtel, E. D.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Materials, Nonmetallic
Report/Patent Number
AIAA PAPER 73-735
Report Number: AIAA PAPER 73-735
Meeting Information
Meeting: Thermophysics Conference
Location: Palm Springs, CA
Start Date: July 16, 1973
End Date: July 18, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A36352
Funding Number(s)
CONTRACT_GRANT: AT(29-2)-2831
Distribution Limits
Public
Copyright
Other

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