Pages that link to "Item:Q2820361"
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The following pages link to Study of different modes of fatigue fracture and durability estimation for compressor disc of gas turbine engine (Q2820361):
Displaying 3 items.
- Damage tolerance analysis of a helicopter component (Q1016282) (← links)
- From probabilistic prediction of fatigue life to a new design approach for gas turbines (Q2086287) (← links)
- Model and method for calculating cyclic damage under high-frequency loading of hourglass-shaped samples (Q6665028) (← links)