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A platform for research: civil engineering, architecture and urbanism
Aircraft plywood tested carefully
Private laboratory tests showed that there is no significant difference in strength and behavior or adhesives used; most fatigue bending failures were wood failures; outer piles gave way before delamination of veneers occurred; conventional plywood product should withstand minimum of 200,000 stress reversals without failure, when stressed not over 25% of static modulus of rupture.
Aircraft plywood tested carefully
Private laboratory tests showed that there is no significant difference in strength and behavior or adhesives used; most fatigue bending failures were wood failures; outer piles gave way before delamination of veneers occurred; conventional plywood product should withstand minimum of 200,000 stress reversals without failure, when stressed not over 25% of static modulus of rupture.
Aircraft plywood tested carefully
Veneers Plywood
Veneers and Plywood ; 46
1952
Article (Journal)
English
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