Author: Harvey G. McComb
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 48
Book Description
A method is presented for analyzing the stresses about a cutout in a circular cylinder of monocoque construction. The method involves the use of so-called perturbation solutions which are superposed on the stress distribution that would exist in the structure with no cutout in such a way as to give the effects of a cutout. The method can be used for any loading case for which the structure without the cutout can be analyzed and is sufficiently versatile to account for stringer and shear reinforcement about the cutout.
Stress Analysis of Circular Semimonocoque Cylinders with Cutouts by a Perturbation Load Technique
Author: Harvey G. McComb
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 48
Book Description
A method is presented for analyzing the stresses about a cutout in a circular cylinder of monocoque construction. The method involves the use of so-called perturbation solutions which are superposed on the stress distribution that would exist in the structure with no cutout in such a way as to give the effects of a cutout. The method can be used for any loading case for which the structure without the cutout can be analyzed and is sufficiently versatile to account for stringer and shear reinforcement about the cutout.
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 48
Book Description
A method is presented for analyzing the stresses about a cutout in a circular cylinder of monocoque construction. The method involves the use of so-called perturbation solutions which are superposed on the stress distribution that would exist in the structure with no cutout in such a way as to give the effects of a cutout. The method can be used for any loading case for which the structure without the cutout can be analyzed and is sufficiently versatile to account for stringer and shear reinforcement about the cutout.
Stresses in a Compressively Loaded Circular Semimonocoque Cylinder with a Cutout
Stress Distributions Caused by Three Types of Loading on a Circular Semimonocoque Cylinder with Flexible Wings
Author: Harvey G. McComb
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 62
Book Description
Equations are derived for the stress distributions caused by three types of loading on infinitely long, circular, semimonocoque cylinders with flexible rings. These external loads can be said to lie in the sheet-stringer surface of the cylinder; that is, they have no radial components. The results, given as formulas for the stringer loads and shear flows in the shell, are of use in the stress analysis of circular semimonocoque cylinders with cutouts. In order to facilitate this application, the formulas can be used to construct tables of influence coefficients giving stringer loads and shear flows in the neighborhood of each particular external load due to a unit magnitude of that load.
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 62
Book Description
Equations are derived for the stress distributions caused by three types of loading on infinitely long, circular, semimonocoque cylinders with flexible rings. These external loads can be said to lie in the sheet-stringer surface of the cylinder; that is, they have no radial components. The results, given as formulas for the stringer loads and shear flows in the shell, are of use in the stress analysis of circular semimonocoque cylinders with cutouts. In order to facilitate this application, the formulas can be used to construct tables of influence coefficients giving stringer loads and shear flows in the neighborhood of each particular external load due to a unit magnitude of that load.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1172
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1172
Book Description
Technical Note
Simplified Procedures and Charts for the Rapid Estimation of Bending Frequencies of Rotating Beams
Author: Robert T. Yntema
Publisher:
ISBN:
Category : Bars (Engineering)
Languages : en
Pages : 692
Book Description
A more exact mode-expansion method used in evaluating the Rayleigh approach is also described. Numerous mode shapes and derivatives obtained in conjunction with the frequency calculations are presented in tabular form.
Publisher:
ISBN:
Category : Bars (Engineering)
Languages : en
Pages : 692
Book Description
A more exact mode-expansion method used in evaluating the Rayleigh approach is also described. Numerous mode shapes and derivatives obtained in conjunction with the frequency calculations are presented in tabular form.
NASA Technical Translation
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 800
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 800
Book Description
An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-stringer Panels with Special Reference to the Influence of the Riveted Connection Between Sheet and Stringer
Author: Benjamin H. Beam
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 312
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 312
Book Description