Inspection Periods Determined from Data of Crack Development and Strength Reduction of an Aircraft Structure Using Static Analysis

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Report Number: ASD TDR 62-391
Author(s): Eggwertz, Sigge
Corporate Author(s): The Aeronautical Research Institute of Sweden (FFA)
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-05
Pages: 26
Contract: AF 61(052)-431
DoD Project: 1367
DoD Task: 136710
Identifier: AD0278171

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Provenance: Bombardier/Aero

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