Author: Michael F. CardPublisher:
ISBN:
Category : Bending
Languages : en
Pages : 44
Book Description
Bending Tests of Large-diameter Stiffened Cylinders Susceptible to General Instability
Author: Michael F. CardPublisher:
ISBN:
Category : Bending
Languages : en
Pages : 44
Book Description
NASA Technical Note
Author: Buckling of Stiffened Cylinders in Axial Compression and Bending
Author: James P. PetersonPublisher:
ISBN:
Category : Axial compression and bending
Languages : en
Pages : 36
Book Description
Buckling data review for stiffened cylinder failures during axial compression and bending.
Bending Tests of Large-diameter Ring-stiffened Corrugated Cylinders
Author: James P. PetersonPublisher:
ISBN:
Category : Bending fatigue
Languages : en
Pages : 44
Book Description
Preliminary Results of Compression Tests on Cylinders with Eccentric Longitudinal Stiffeners
Author: Michael F. CardThe General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure
Author: John N. DicksonPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124
Book Description
Influence of Ring Stiffeners on Instability of Orthotropic Cylinders in Axial Compression
Author: David L. BlockPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 32
Book Description
General Instability of Orthotropically Stiffened Cylinders
Author: C. LakshmikanthamPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 58
Book Description
As part of a general program to determine the applicability of linear orthotropic theory to the design of cylindrical shells under various loading conditions, a theoretical and experimental investigation was performed on the general instability of orthotropic cylinders under bending and combined axial compression and bending loading. Based on a simple approximation for the asymmetric buckling pattern, theoretical results suitable for design use were obtained for the buckling of orthotropic cylinders for both bending and combined loading conditions. It was shown that the buckling stress for orthotropic cylinders under bending or axial compression loading are equal which agrees with previous results for isotropic cylinders. Theoretical results were evaluated by means of a series of careful experiments performed on orthotropically stiffened cylinders designed to fail in the elastic general instability mode. For both bending loading and the combined axial and bending loading condition, experimental results were in good agreement with the theory.
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Some Investigations of the General Instability of Stiffened Metal Cylinders
Author: Daniel Guggenheim Aeronautical LaboratoryPublisher:
ISBN:
Category : Bending
Languages : en
Pages : 656
Book Description
This is the sixth of a series of report covering an investigation of the general instability problem by the California Institute of Technology. This report summarizes the work that has been carried on in the experimental investigation of the problem of general instability of stiffened metal cylinders subjected to combined bending and transverse shear.