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Small-Crack Effects in High-Strength Aluminum Alloys

机译:高强度铝合金的小裂纹效应

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The National Aeronautics and Space Administration and the Chinese AeronauticalEstablishment participated in a Fatigue and Fracture Mechanics Cooperative Program. The program objectives were to identify and characterize crack initiation and growth of small cracks (10 microns to 2 mm long) in commonly used

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