Metal Matrix Composites for High Temperature Application.
Interim progress rept. for the year 1971,
WATERVLIET ARSENAL N Y
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The objective of the program is to develop fabrication techniques and to characterize high strength-high temperature filament reinforced superalloys for application as turbine blade materials. Using the sessile drop and infiltration techniques, the compatibility of W and SiC filaments against castable superalloys including Mar M200, Mar M302, Mar M322, J-1650, and IN-100 was investigated. Author
- Laminates and Composite Materials
- Jet and Gas Turbine Engines