Author: Walter Ramberg
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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
Author: Walter Ramberg
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 782
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 782
Book Description
Strength of Beams Under Transverse Loads
Author: William Allan
Publisher:
ISBN:
Category : Strains and stresses
Languages : en
Pages : 134
Book Description
Publisher:
ISBN:
Category : Strains and stresses
Languages : en
Pages : 134
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Notes and Tables for Use in the Analysis of Supersonic Flow
Author:
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 594
Book Description
This document is a compilation of formulas, tables, and curves for use in the analysis of supersonic flow.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 594
Book Description
This document is a compilation of formulas, tables, and curves for use in the analysis of supersonic flow.
Air Service Information Circular
Author:
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 1636
Book Description
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 1636
Book Description
National Bureau of Standards Handbook
Author: Sherman F. Booth
Publisher:
ISBN:
Category : Industrial safety
Languages : en
Pages : 974
Book Description
Publisher:
ISBN:
Category : Industrial safety
Languages : en
Pages : 974
Book Description
Effect of Aging Aircraft Structures on Magnesium Parts
Author: A. W. Winston
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 716
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.
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 716
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
Author: J. A. Newlin
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 192
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 192
Book Description
The Analysis and Design of Airplane Wing Beams Subjected to Combined Axial and Transverse Loads
Author: Joseph Shipley Newell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 142
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 142
Book Description