Strength of Wing Beams Under Axial and Transverse Loads

Strength of Wing Beams Under Axial and Transverse Loads PDF Author: Walter Ramberg
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

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Book Description
Wing beams of six designs, referred to as types A to F, were tested under axial compressive loads, transverse loads, and combined axial and transverse loads. Two specimens of each type were loaded in compression only. Four specimens of each type were loaded by combined axial and transverse load wit hthe location of the load points so chosen as to produce failure in the central portion of the beam. The remaining two specimens of each type were loaded by transverse loads so chosen as to produce failure by bending in the central portion for one specimen and by shear in the end portions for the other.

Strength of Wing Beams Under Axial and Transverse Loads

Strength of Wing Beams Under Axial and Transverse Loads PDF Author: Walter Ramberg
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

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Book Description
Wing beams of six designs, referred to as types A to F, were tested under axial compressive loads, transverse loads, and combined axial and transverse loads. Two specimens of each type were loaded in compression only. Four specimens of each type were loaded by combined axial and transverse load wit hthe location of the load points so chosen as to produce failure in the central portion of the beam. The remaining two specimens of each type were loaded by transverse loads so chosen as to produce failure by bending in the central portion for one specimen and by shear in the end portions for the other.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 782

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Strength of Beams Under Transverse Loads

Strength of Beams Under Transverse Loads PDF Author: William Allan
Publisher:
ISBN:
Category : Strains and stresses
Languages : en
Pages : 134

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274

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Notes and Tables for Use in the Analysis of Supersonic Flow

Notes and Tables for Use in the Analysis of Supersonic Flow PDF Author:
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 594

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Book Description
This document is a compilation of formulas, tables, and curves for use in the analysis of supersonic flow.

Air Service Information Circular

Air Service Information Circular PDF Author:
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 1636

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National Bureau of Standards Handbook

National Bureau of Standards Handbook PDF Author: Sherman F. Booth
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ISBN:
Category : Industrial safety
Languages : en
Pages : 974

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Effect of Aging Aircraft Structures on Magnesium Parts

Effect of Aging Aircraft Structures on Magnesium Parts PDF Author: A. W. Winston
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 716

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Book Description
The forms in which magnesium alloys may be encountered are castings, extrusions, forgings, and sheet. The alloys commonly used in aircraft structures in the various forms and the effects of the aging treatment are discussed under separate headings below.

The Design of Airplane Wing Ribs

The Design of Airplane Wing Ribs PDF Author: J. A. Newlin
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ISBN:
Category : Aeronautics
Languages : en
Pages : 192

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The Analysis and Design of Airplane Wing Beams Subjected to Combined Axial and Transverse Loads

The Analysis and Design of Airplane Wing Beams Subjected to Combined Axial and Transverse Loads PDF Author: Joseph Shipley Newell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 142

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Book Description