MODE I INTERLAMINAR FRACTURE TOUGHNESS OF COMPOSITES USING SLENDER DOUBLE CENTILEVERED BEAM SPECIMENS.

被引：0
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作者：
Keary, Paul E. [1 ]
Ilcewicz, Larry B. [1 ]
Shaar, Casey [1 ]
Trostle, Jess [1 ]
机构：
[1] Boeing Commercial Airplane Co,, Seattle, WA, USA, Boeing Commercial Airplane Co, Seattle, WA, USA
来源：
| 1600年 / 19期
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摘要：
COMPOSITE MATERIALS
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