An exploded view of a GLARE hybrid sheet

Autor/Urheber:

Jenn-Ming Yang, Thomas H. Hahn, Hyoungseock Seo, Po-Yu Chang, and Po-Ching Yeh Mechanical and Aerospace Engineering Department Materials Science and Engineering Department University of California at Los Angeles

Los Angeles, CA 90024-1597

Shortlink:

https://dewiki.de/b/2e08e1

Quelle:

Wikimedia Commons

Größe:

1746 x 820 Pixel (153716 Bytes)

Beschreibung:

A component view of a GLARE3-3/2 hybrid sheet. There are three layers of aluminum alternating with two layers of glass fiber. In a GLARE3 grade, each glass fiber layer has two plies: one oriented at zero degrees, and the other oriented at ninety degrees.

Lizenz:

Public domain

Credit:

Damage Tolerance and Durability of Fiber-Metal Laminates for Aircraft Structures Figure 1. A Cross-Ply GLARE 3-3/2 Laminate http://www.tc.faa.gov/its/worldpac/techrpt/ar1018.pdf

DOT/FAA/AR-10/18 U.S. Department of Transportation Federal Aviation Administration Air Traffic Organization NextGen & Operations Planning Office of Research and Technology Development

Washington, DC 20591

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