Supplement to fatigue tests of glass-fabric-base laminates subjected to axial loading

Public Deposited

Citeable URL: https://ir.library.oregonstate.edu/concern/defaults/bv73c412q

Descriptions

Attribute Name	Values
Creator	Werren, Fred 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 notched specimens. The results of a few bearing tests at 0° loading are also included. Data from the individual tests, and S-N curves based on these data, are presented. The S-N curves indicate how fatigue properties are affected by factors such as direction of loading, stress concentrations, and wet conditions. This report is one of a series issued in cooperation with the ANC-17 Panel on Plastics for Aircraft of the Departments of the Air Force, Navy, and Commerce.
Resource Type	Technical Report
Date Available	2006-06-12T16:24:41+00:00
Date Issued	1962
Series	Report (Forest Products Laboratory (U.S.))
Subject	Airplanes -- Materials Laminated plastics -- Fatigue Axial loads
Rights Statement	Copyright Not Evaluated
Publisher	Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory
Language	English [eng]
File Format	application/pdf
File Extent	2819823 bytes
Digitization Specifications	Scanned at 600 DPI using a Cannon DR-9080C in TIF format. PDF generated through Capture Perfect using OmniPage 14 Pro for textual OCR.
Replaces	http://hdl.handle.net/1957/2153

Thumbnail	Title	Date Uploaded	Visibility	Actions
	FPL_1823-Bocr.pdf	2017-09-26	Public	Download