Failure Processes in Metal Matrix Composites. Phase II.
Final rept. 1 Oct-31 Dec 73 on Phase 2,
GENERAL ELECTRIC CO CINCINNATI OHIO AIRCRAFT ENGINE GROUP
Pagination or Media Count:
BoronAluminum BAl composite blades were consolidated and impacted by RTV birds. Failure responses were observed. The blade deflections as determined by high speed movies were compared with calculated values generated from and AFML model and gave good agreement. Analyses of the strain gage responses yield inherent stress levels, resonant frequencies and logarithmic decrement of these blades. Author
- Laminates and Composite Materials
- Jet and Gas Turbine Engines