Deflections of AN Inflated Circular-Cylindrical Cantilever Beam

The problem of determining the hydrodynamic entrance length in a rectangular channel is solved by the method of linearizing the Navier-Stokes equation. The resulting equation is regarded as an equation to generate a mathematical expression for the axial velocity in the entire region, making smooth transition from a uniform profile to the fully developed one. From this expression, the entrance length, defined as where 99 per cent of the fully developed center-line velocity is attained, is calculated for channels of six aspect ratios. The pressure drops are also calculated and presented herein. A comparison is made with the limited amount of experimental and theoretical data.

Hydrodynamic Entrance Lengths for Incompressible Laminar Flow in Rectangular Ducts

Buckling of quasi-perfect cylindrical shell under axial compression: A combined experimental and numerical investigation

Nomenclature D = flexural stiff ness of shell wall Et*/[ 12(1 - */2)] E = Young's modulus of shell wall material L = axial length of cylinder or cone / = slant length of cone n = number of circumferential waves in cone buckled under external pressure n = number of circumferential waves in equivalent cylinder buckled under external pressure PO = critical axial compression load p = total axial load at buckling P = uniform internal or external hydrostatic pressure POT, PQ — critical external pressure pe = critical external pressure for equivalent cylinder R = cylinder radius RI = radius of small end of cone Rz = radius of large end of cone t = shell wall thickness a = semivertex angle of cone v = Poisson's ratio of wall material Pav = average radius of curvature of cone (Ri + Rz)/% coso;

Elastic stability of thin-walled cylindrical and conical shells under combined internal pressure and axial compression

An experimental study of the plastic buckling of circular cylinders in pure bending

The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal Pressure

In 1951, an extensive review of the literature indicated that only a limited amount of test data was available to evaluate the effect of internal pressure on the stability of unstiffened and stiffened circular cylindrical shells. In addition, data on the postbuckling strength of stiffened cylinders were also limited. Because of the importance of the cylindrical shell in missile construction, an extensive investigation was initiated to provide such data. The present paper includes a description of the test techniques used in these investigations and some conclusions derived from the results.

Model investigations of unstiffened and stiffened circular shells

The Effect of Internal Pressure on the Buckling Stress of Thin-Walled Circular Cylinders Under Combined Axial Compression and Torsion

The Bending Stability of Thin-Walled Unstiffened Circular Cylinders Including the Effects of Internal Pressure

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The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal Pressure

Model investigations of unstiffened and stiffened circular shells

The Effect of Internal Pressure on the Buckling Stress of Thin-Walled Circular Cylinders Under Combined Axial Compression and Torsion

The Bending Stability of Thin-Walled Unstiffened Circular Cylinders Including the Effects of Internal Pressure