Author: John N. DicksonPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124
Book Description
The 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
On the General Instability of Ring-stiffened Cylindrical Shells Under the Action of Radial External Pressure and Axial Compression
Author: Sesto Joseph VocePublisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 126
Book Description
The 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
On the Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression
Author: Josef SingerPublisher:
ISBN:
Category :
Languages : en
Pages : 55
Book Description
The eccentricity effect of stiffeners is studied for stiffened cylindrical shells under axial compression. Classical simple supports and classical clamped ends are considered. A detailed physical explanation of the causes of the eccentricity effect and its behavior is proposed and verified by computations for 350 typical shells. As for buckling under hydrostatic pressure and torsion studied earlier, the behavior of the eccentricity effect in the case of axial compression also depends very strongly on the geometry of the shell, represented by the Batdorf parameter, while the geometry of the stiffeners only influences its magnitude. Inversion of eccentricity effect occurs at very low Z, but for practical dimensions outside stringers always stiffen the shell more than inside ones. The eccentricity effect has a pronounced maximum at practical values of Z, and the behavior of the eccentricity effect is very similar for clamped and simply supported shells. Rings, which are much less effective stiffeners than stringers under axial compression, are also considered. Results are compared with those of other investigators. (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.
The Stability Under Axial Compression and Lateral Pressure of Circular-cylindrical Shells with a Soft Elastic Core
Author: Paul SeidePublisher:
ISBN:
Category :
Languages : en
Pages : 57
Book Description
The stability under axial compression and lateral pressure of a finite circular-cylindrical shell with an elastic core is treated by means of Donnell's equations. The stability criterion is investigated in detail for the general cylinder under axial compression or lateral pressure and for a particular cylinder under combined loading. Comparisons are made with available experimental data. (Author).
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Linear Stability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression
Author: Tien-Yu TsuiPublisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Linear stability of eccentrically stiffened cylindrical shells under axial compression has been investigated in the paper with an aim to establish the parameter ranges for the prevailing buckling modes. Charts delineating the zones of prevailing modes are presented in a parameter plane. Useful approximate relations are given for the bounds on parameters to predict a buckling mode for a shell in the moderate length range. (Author).
Author: 
Author: Arie van der Neut