Author: Manuel Stein
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 24
Book Description
A nondimensional chart is presented for the theoretical critical stress in torsion of simply supported cylinders stiffened by identical, equally spaced, torsionally weak rings. The results are obtained by solving the equation of equilibrium by means of the Galerkin method. Comparison of the theoretical results wit hthe experimental results indicates that ring-stiffened cylinders buckle on the average, at a buckling stress about 15 percent below the theoretical buckling stress presented.
Critical Stress of Ring-stiffened Cylinders in Torsion
Author: Manuel Stein
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 24
Book Description
A nondimensional chart is presented for the theoretical critical stress in torsion of simply supported cylinders stiffened by identical, equally spaced, torsionally weak rings. The results are obtained by solving the equation of equilibrium by means of the Galerkin method. Comparison of the theoretical results wit hthe experimental results indicates that ring-stiffened cylinders buckle on the average, at a buckling stress about 15 percent below the theoretical buckling stress presented.
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 24
Book Description
A nondimensional chart is presented for the theoretical critical stress in torsion of simply supported cylinders stiffened by identical, equally spaced, torsionally weak rings. The results are obtained by solving the equation of equilibrium by means of the Galerkin method. Comparison of the theoretical results wit hthe experimental results indicates that ring-stiffened cylinders buckle on the average, at a buckling stress about 15 percent below the theoretical buckling stress presented.
Critical Stress of Ring-stiffened Cylinders in Torsion
Author: Manuel Stein
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 17
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 17
Book Description
Method for Determining the Frequency-response Characteristics of an Element of System from the System Transient Output Response to a Known Input Function
Author: Charles W. Matthews
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 196
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 196
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 532
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 532
Book Description
Influence of Ring Stiffeners on Instability of Orthotropic Cylinders in Axial Compression
Author: David L. Block
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 32
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Bibliography of Technical Reports
Stability Analysis of Plates and Shells
Author:
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
Book Description
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
Book Description