NASA NTRS · 19710054459
Fatigue crack propagation in stiffened panels
Abstract
Fatigue crack propagation in Al alloy panels stiffened with bolted and integral stringers, determining stress intensity factor/crack growth rate relationship
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Poe, C. C., Jr.. 1971-01-01. Fatigue crack propagation in stiffened panels. https://ntrs.nasa.gov/citations/19710054459
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