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[American Institute of Aeronautics and Astronautics 15th Structural Dynamics and Materials Conference - Las Vegas,NV,U.S.A. (17 April 1974 - 19 April 1974)] 15th Structural Dynamics and Materials Conference - Development and application of a fatigue-crack-propagation model based on the inverse hyperbolic tangent function

✍ Scribed by DAVIES, K.; FEDDERSEN, C.

Book ID: 121024495
Publisher: American Institute of Aeronautics and Astronautics
Year: 1974
Weight: 443 KB
Category: Article
DOI: 10.2514/6.1974-368

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