Author: Karl Schüssler
Publisher:
ISBN:
Category : Duralumin
Languages : en
Pages : 662
Book Description
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.
The Behavior Under Shearing Stress of Duralumin Strip with Round, Flanged Holes
Author: Karl Schüssler
Publisher:
ISBN:
Category : Duralumin
Languages : en
Pages : 662
Book Description
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.
Publisher:
ISBN:
Category : Duralumin
Languages : en
Pages : 662
Book Description
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
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Technical Memorandum - National Advisory Committee for Aeronautics
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 698
Book Description
Chiefly translations from foreign aeronautical journals.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 698
Book Description
Chiefly translations from foreign aeronautical journals.
Technical Memorandums
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description
Chiefly translations from foreign aeronautical journals.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description
Chiefly translations from foreign aeronautical journals.
Index of Aircraft Structures Research Reports
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
Book Description
Subject and Author Index of the Technical Memorandums [nos. 1-1062] of the U.S. National Advisory Committee for Aeronautics
Author: Chrysler Corporation. Engineering Library
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 132
Book Description
Wartime Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 308
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 308
Book Description
Catalogue of the Public Documents of the ... Congress and of All Departments of the Government of the United States for the Period from ... to ...
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2660
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2660
Book Description
Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 310
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 310
Book Description