The effect of flight-by-flight load and temperature sequences on residual static strength of notched specimens in CM003 (RR58) aluminium alloy

The effect of flight-by-flight load and temperature sequences on residual static strength of notched specimens in CM003 (RR58) aluminium alloy

F. E. Kiddle
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1373
Date: 1977

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