Author: NASA Symposium on Instability of Shell StructuresPublisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 800
Book Description
Collected Papers on Instability of Shell Structures, 1962
Author: NASA Symposium on Instability of Shell StructuresPublisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 800
Book Description
Collected Papers on Instability of Shell Structure, 1962
Author: Publisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 0
Book Description
Collected Papers on Instability of Shell Structure, 1962
Author: Publisher:
ISBN:
Category : Elastic plates and shells
Languages : en
Pages : 790
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 936
Book Description
NASA Technical Note
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 478
Book Description
Structural Design and Analysis
Author: C. C. ChamisPublisher: Elsevier
ISBN: 148321673X
Category : Technology & Engineering
Languages : en
Pages : 370
Book Description
Structural Design and Analysis
Stability Analysis of Plates and Shells
Author: Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 460
Book Description
Applied Mechanics Reviews
Author: Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Book Description
The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression
Author: John N. DicksonPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 44
Book Description
A method is presented to determine the general instability load of a ring-stiffened corrugated cylinder under axial compression. This method is developed using linear small deflection theory. The stiffness properties of the rings are uniformly distributed along the cylinder and the eccentricity of the rings with respect to the corrugation centerline is taken into account. Analytical and experimental results are compared. In this comparison good agreement is obtained for cylinders loaded in pure compression. For the cylinders subjected to bending or a combination of bending and compression the analytical calculations are conservative. A computer program for the application of this method has been developed. The program and an explanation of its notation are included in this report.
Structural Design Concepts
Author: Louis Albert ScipioPublisher:
ISBN:
Category : Building materials
Languages : en
Pages : 186
Book Description
