An Evaluation of MAT_224 for Simulation of Impact and Failure Part I: A Scaling Approach for Modeling AMS 4911 Titanium Plates with Different Thickness and Properties

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An Evaluation of MAT_224 for Simulation of Impact and Failure Part I: A Scaling Approach for Modeling AMS 4911 Titanium Plates with Different Thickness and Properties

2017-01-01

File Language:

English

Details

Publication/ Report Number:

DOT/FAA/TC-17/43
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Format:

PDF
Collection(s):

FAA Technical Library
Main Document Checksum:

urn:sha256:c5336d9ca7e40b7ff88d7df96a6d0f3cdf000dfebf3047af01841ee924041425
Download URL:

https://rosap.ntl.bts.gov/view/dot/57726/dot_57726_DS1.pdf
File Type:

[PDF - 2.93 MB ]

File Language:

English

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Details

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