SAE Technical Paper Series 1967
DOI: 10.4271/670822
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Compatibility Considerations for Metal-Matrix Composites

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1970
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“…Engines have been designed to eliminate deposit-prone components, and to include an erosion margin in aerodynamic blade design (13). Blade design, influenced by the results of erosion studies on impingement angle and material modulus, shows promise to help minimize the dust problem (57). Gas turbine regenerator design might anticipate a certain degree of fouling from dust deposits by over-surfacing so that the effects of fouling are counteracted (58).…”
Section: Field Testsmentioning
confidence: 99%
“…Engines have been designed to eliminate deposit-prone components, and to include an erosion margin in aerodynamic blade design (13). Blade design, influenced by the results of erosion studies on impingement angle and material modulus, shows promise to help minimize the dust problem (57). Gas turbine regenerator design might anticipate a certain degree of fouling from dust deposits by over-surfacing so that the effects of fouling are counteracted (58).…”
Section: Field Testsmentioning
confidence: 99%