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Smith, Bert L.
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Residual Strength of an Aluminum Panel with a Centric Hole and One Cracked Ligament

Published 1999-04-20 by SAE International in United States
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Predicting Fatigue Crack Growth on Aircraft Structures

Published 1981-02-01 by SAE International in United States
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A Computer Program for Predicting Fatigue Crack Propagation

Published 1981-02-01 by SAE International in United States
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Damage Tolerance of Honeycomb Sandwich Composite Panels

Published 2002-04-16 by SAE International in United States
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Summary of the Effect of Multiple Site Damage on the Linkup Strength of 2024-T3 Aluminum Panels

Published 2002-04-16 by SAE International in United States
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Thermal Properties of Thin Laminated Composite Plates

Published 1976-02-01 by SAE International in United States
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Simplified Methods for Determining Stresses and Deflections of Thin Laminated Composite Plates

Published 1977-02-01 by SAE International in United States
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