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Summary
| Description |
English: 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. |
| Date | |
| Source |
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 |
| Author |
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 |
Licensing
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This image or file is a work of a Federal Aviation Administration employee, taken or made as part of that person's official duties. As a work of the U.S. federal government, the image is in the public domain in the United States.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 02:09, 25 December 2018 | | 1,746 × 820 (150 KB) | D271l | User created page with UploadWizard |
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