The Behavior Under Shearing Stress of Duralumin Strip with Round, Flanged Holes

The Behavior Under Shearing Stress of Duralumin Strip with Round, Flanged Holes
Author: Karl Schüssler
Publisher:
Total Pages: 662
Release: 1934
Genre: Duralumin
ISBN:

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This report presents the results of an investigation to determine the behavior of dural strip with flanged holes in the center when subjected to shear stresses. They buckle under a certain load just as a flat sheet. There is one optimum hole spacing and a corresponding buckling load in shear for each sheet width, sheet thickness, and flange form. Comparison with non-flanged sheets revealed a marked increase of buckling load in shear due to the flanging and a slightly greater displacement. Strips were clamped between two stationary end rails and one sliding center rail at which the shear is applied. The force was measured with a tension stirrup up to 20 tons and a compression dynamometer up to 10 tons. The displacement was recorded with the Zeiss dial gauge. The following were investigated: 1) effect of strip width; 2) strip thickness; 3) diameter of flanging; 4) depth of flanging; 5) and hole distance.

Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 1370
Release: 1949
Genre: Aeronautics
ISBN:

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Technical Memorandums

Technical Memorandums
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 442
Release: 1934
Genre: Aeronautics
ISBN:

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Chiefly translations from foreign aeronautical journals.

Index of Aircraft Structures Research Reports

Index of Aircraft Structures Research Reports
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 48
Release: 1947
Genre: Airplanes
ISBN:

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Wartime Report

Wartime Report
Author:
Publisher:
Total Pages: 308
Release:
Genre: Aeronautics
ISBN:

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Wartime Report

Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 310
Release:
Genre: Aeronautics
ISBN:

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