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Start Over Partner UNT Libraries Government Documents Department Collection National Advisory Committee for Aeronautics Collection Year 1953 Month October Day 13th

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Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine 2: Root Design Alterations (open access)

Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine 2: Root Design Alterations

Report presenting engine evaluation tests of twelve sets of cermet turbine blades. The first five runs were similar to previous engine tests, but the remaining ones were modified based on information gained during the first runs.
Date: October 13, 1953
Creator: Meyer, A. J., Jr.; Deutsch, G. C. & Morgan, W. C.
System: The UNT Digital Library