Skip to Main Content
Skip Nav Destination
ASTM Selected Technical Papers
Test Methods for Compression Members
By
Committee E-1
Committee E-1
Search for other works by this author on:
ISBN-10:
0-8031-6174-3
ISBN:
978-0-8031-6174-0
No. of Pages:
218
Publisher:
ASTM International
Publication date:
1967

A novel method for fabricating “near-perfect” circular cylinders of photoelastic plastic is presented. The spin-casting technique was found to yield circular cylinders having thickness variations as low as ±0.0006 in., and capable of maintaining this tolerance on shells with radius-to-thickness ratios in the range of 100 ⩽ R/t ⩽ 600. The cylinders generally were found to buckle within 10 per cent of the classical computed load, and within only a few per cent of the reduced value taking into account the clamped end constraints. This represents an increase over previous experimental data. Buckling was completely elastic, and, as a result, repeatability of the buckling load and buckling process was observed for as many as 20 tests on any one shell. Experimental evidence of the unstable states occupied by the shell during the buckling process was found by photographing the change in the 45-deg isoclinics with wave shape. Shell alignment, end constraints, and the method of applying a uniform compressive end load on the cylinder are also discussed. Although no new techniques were employed, the methods used were found reliable and accurate.

1.
Hoff
,
N. J.
,
Madsen
,
W. A.
, and
Mayers
,
J.
, “
The Postbuckling Equilibrium of Axially Compressed Circular Cylindrical Shells
,” SUDAER No. 221,
Department of Aeronautics and Astronautics, Stanford University
,
1965
.
2.
Koiter
,
W. T.
, “
The Effect of Axisymmetric Imperfections on the Buckling of Cylindrical Shells under Axial Compression
,”
Proceedings
,
Royal Netherlands Academy of Sciences
,
Amsterdam
, Series B, Vol
66
, No.
5
,
1963
.
3.
Almroth
,
B. O.
, “
Influence of Edge Conditions on the Stability of Axially Compressed Cylindrical Shells
,” NASA CR-161,
National Aeronautics and Space Administration
,
1965
.
4.
Mönch
,
E.
, “
Photoelastic Investigation of Shells by Means of a Model in Whose Middle Surface a Semi-Transparent Mirror Layer is Embedded
,”
IXe Congrès International de Mécanique Appliquée Actes
,
Bruxelles
, Tome
VIII
,
1957
, pp. 384-394.
5.
Tennyson
,
R. C.
, “
A Note on the Classical Buckling Load of Circular Cylinrical Shells under Axial Compression
,”
Journal
, American Institute of Aeronautics and Astronautics, Vol
1
, No.
2
,
1963
.
6.
Tennyson
,
R. C.
, “
An Experimental Investigation of the Buckling of Circular Cylindrical Shells in Axial Compression Using the Photoelastic Technique
,” UTIAS Report No. 102,
University of Toronto Institute for Aerospace Studies
,
1964
.
7.
Gorman
,
D.
, and
Evan-Iwanowski
,
R. M.
, “
Photoelastic Analysis of Prebuckling Deformations of Cylindrical Shells
,”
Journal
, American Institute of Aeronautics and Astronautics, Vol
3
, No.
10
,
1965
.
8.
Müller
,
R. K.
, “
The Influence of Measuring Current and Preheating on Measurements on Resins with Electric-Resistance Strain Gages
,”
Journal of Experimental Mechanics
, Society for Experimental Stress Analysis, Vol
5
, No.
11
,
1965
.
9.
Weingarten
,
V. I.
,
Morgan
,
E. J.
, and
Seide
,
P.
, “
Elastic Stability of Thin-Walled Cylindrical and Conical Shells under Axial Compression
,”
Journal
, American Institute of Aeronautics and Astronautics, Vol
3
, No.
6
,
1965
.
10.
Almroth
,
B. O.
,
Holmes
,
A. M. C.
, and
Brush
,
D. O.
, “
An Experimental Study of the Buckling of Cylinders under Axial Compression
,”
Journal of Experimental Mechanics
, Society for Experimental Stress Analysis, Vol
4
, No.
9
,
1964
.
11.
Coppa
,
A. P.
, “
Measurement of Initial Geometrical Imperfections of Cylindrical Shells
,”
Journal
, American Institute of Aeronautics and Astronautics, Vol
4
, No.
1
,
1966
.
12.
Babcock
,
C. D.
, and
Sechler
,
E. E.
, “
The Effect of Initial Imperfections on the Buckling Stress of Cylindrical Shells
,” NASA TN D-2005,
National Aeronautics and Space Administration
,
1963
.
13.
Leonard
,
R. W.
, “
Comments on a Note on the Classical Buckling Load of Circular Cylindrical Shells under Axial Compression
,”
Journal
, American Institute of Aeronautics and Astronautics, Vol
1
, No.
9
,
1963
.
This content is only available via PDF.
You do not currently have access to this chapter.
Close Modal

or Create an Account

Close Modal
Close Modal