ASD Technical Report, Numéro 63,Partie 195Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963 |
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Aeronautical Systems Division ambient and high Ambient Unspecified analysis of ambient anisotropic anisotropic nature anisotropic properties anisotropies are examined annealing temperature application of pyrolytic basal plane characteristics of pyrolytic compression cones crystallites data on pyrolytic decrease density deposition temperature design limitations designer exploit diffusion controlled rate Effect of Deposition Effect of Heat electrical conductivity electrical resistivity gas pressure graphite are discussed graphite is presented growth Heat Treatment High Temperature Materials HIGH TEMPERATURE PROPERTIES high temperature region hkl reflections increases J. R. Armstrong layer planes Lockheed Aircraft Corp lytic graphite mandrel material deposited maximum mechanical anisotropies microstructure nucleated oxidation theories process variables properties are analyzed Properties of Pyrolytic pyro Pyrolytic Carbon Pyrolytic Graphite Deposit pyrolytic graphite requires reaction controlled reaction mechanisms region are summarized specimen stagnation point supersaturation Table TEMP temperature on material temperature property data tensile strength thermal conductivity thermal shock tion view toward aid Wright-Patterson AFB