A Potential Oxide/Oxide Ceramic Matrix Composite for Gas Turbine Applications.
類似資料:
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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テクニカルペーパー
Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications
National Aeronautics and Space Administration |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |