Add to ORKGDeflections and internal loading distribution of circular cylindrical shell supported ring frames with out-of-plane loading
Determining general instability load of ring stiffened corrugated cylinder under axial compression b...
In the present part I of a series of reports on the inward bulge type buckling of monocoque cylinder...
Testing machine influence on buckling of cylindrical shells under axial compressio
Thirty-four circular cylinders stiffened by heavy rings were loaded to failure in combined bending a...
The formulas given in this report provide a simplified method for the stress-analysis of fuselage bu...
Twenty-five ring-stiffened circular cylinders were loaded to failure in bending. The results are pre...
Displacement results of plane boundary collocation analysis are given for various locations on the i...
Equations are derived for the stress distributions caused by three types of loading on infinitely lo...
At the ends of a monocoque fuselage concentrated axial forces in the skin must generally be taken up...
The present study treats as a typical example a ring the center line of which is produced by the int...
Orthotropic shell theory to develop working tools to predict instability in stiffened circular cylin...
Computer programs for determining response of beams and rings to high intensity, short duration load...
Buckling and postbuckling tests of ring-stiffened circular cylinders loaded to failure by uniform ex...
This report is a compilation of previously published articles on formulas and methods of calculation...
Influence of boundary conditions of buckling load of cylindrical shells under axial compressio
Determining general instability load of ring stiffened corrugated cylinder under axial compression b...
In the present part I of a series of reports on the inward bulge type buckling of monocoque cylinder...
Testing machine influence on buckling of cylindrical shells under axial compressio
Thirty-four circular cylinders stiffened by heavy rings were loaded to failure in combined bending a...
The formulas given in this report provide a simplified method for the stress-analysis of fuselage bu...
Twenty-five ring-stiffened circular cylinders were loaded to failure in bending. The results are pre...
Displacement results of plane boundary collocation analysis are given for various locations on the i...
Equations are derived for the stress distributions caused by three types of loading on infinitely lo...
At the ends of a monocoque fuselage concentrated axial forces in the skin must generally be taken up...
The present study treats as a typical example a ring the center line of which is produced by the int...
Orthotropic shell theory to develop working tools to predict instability in stiffened circular cylin...
Computer programs for determining response of beams and rings to high intensity, short duration load...
Buckling and postbuckling tests of ring-stiffened circular cylinders loaded to failure by uniform ex...
This report is a compilation of previously published articles on formulas and methods of calculation...
Influence of boundary conditions of buckling load of cylindrical shells under axial compressio
Determining general instability load of ring stiffened corrugated cylinder under axial compression b...
In the present part I of a series of reports on the inward bulge type buckling of monocoque cylinder...
Testing machine influence on buckling of cylindrical shells under axial compressio