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Creator:: Kimball, Kenneth Edmund and Forest Products Laboratory (U.S.)
Abstract:: This report presents the results of tests made to determine the effect of different types of configurations and notches on the tensile strength and fatigue strength of a typical epoxy laminate. Tension tests were first made of 13 groups of specimens having different forms. Based on the results of the...
Resource Type:: Technical Report
Full Text:: if the material is notch sensitive, then it would be expected that the fatigue strength of the

Creator:: Werren, Fred and Forest Products Laboratory (U.S.)
Abstract:: This report presents the results of fatigue tests of an epoxide laminate subjected to axial loading. Direct stress tests were made at 0°, 15°, 30°, and 45° to the warp direction. Stress was applied at a frequency of 900 cycles per minute at zero mean stress on both unnotched and...
Resource Type:: Technical Report
Full Text:: . About 40 percent of the laminated material was uses for tests of mechani- cal and fatigue properties

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: This report has been prepared as a supplement to Forest Products Laboratory Report No. 1823, "Fatigue Tests of Glass-Fabric-Base Laminates Subjected to Axial Loading." It presents a correlation of the fatigue data in the basic report with stress-rupture data on the same material reported in Forest Products Laboratory Report No....
Resource Type:: Technical Report
Full Text:: material reported in Forest Products Laboratory Report No. 1839, "Stress-Rupture Tests of a Glass-Fabric

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed August 1958. Original report issued May 1952.
Resource Type:: Technical Report
Full Text:: laminates was parallel-laminated with two types of resin as follows: One laminate was made with a laminating

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Revised April 1943. Publication restriction has been removed. This report is one of a series issued in cooperation with the Army Air Forces and the Bureau of Aeronautics under the supervision of the Aeronautical Board.
Resource Type:: Technical Report
Full Text:: 76 18 : 80 : 85 2 • 5-Thickness of laminated plastic material (in molding pressure direction

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