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Volumn 20, Issue 4, 1999, Pages 523-532
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Design, analysis and testing of ceramic components for an advanced military expendable turbojet engine
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Author keywords
[No Author keywords available]
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Indexed keywords
COMPUTER SIMULATION;
HIGH TEMPERATURE PROPERTIES;
MOLDING;
NOZZLES;
RADIAL FLOW;
ROTORS;
SILICON NITRIDE;
TURBOJET ENGINES;
WEAR RESISTANCE;
HIGH TEMPERATURE BRAZED ROTOR/SHAFT JOINTS;
HYBRID MOLDING PROCESS;
MONOLITHIC SILICON NITRIDE TURBINE COMPONENTS;
CERAMIC MATERIALS;
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EID: 0033343332
PISSN: 01966219
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Article |
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Times cited : (1)
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References (1)
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