Fiberglas-laminate facing and paper honeycomb core sandwich material tested in shear

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Citeable URL: https://ir.library.oregonstate.edu/concern/defaults/fq977z62s

Descriptions

Attribute Name	Values
Creator	Forest Products Laboratory (U.S.) Werren, Fred
Abstract	This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board.
Resource Type	Technical Report
Date Available	2006-04-17T18:13:21+00:00
Date Issued	1949-02
Series	Report (Forest Products Laboratory (U.S.)) Fatigue of sandwich constructions for aircraft
Subject	Shear (Mechanics) Sandwich construction -- Testing Airframes -- Fatigue
Declaração de direitos	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	3851568 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/1957/1671

Miniatura	Título	Data de carga	Acesso	Ações
	FPL_1559-Gocr.pdf	2017-09-26	Público	Baixar