Skip to Main Content
Skip Nav Destination
ASTM Selected Technical Papers
Compression Testing of Homogeneous Materials and Composites
By
R Chait
R Chait
1
Army Materials and Research Mechanics Center
,
Watertown, Mass. 02172
;
symposium co-chairman and co-editor
.
Search for other works by this author on:
R Papirno
R Papirno
2
Army Materials and Research Mechanics Center
,
Watertown, MA, symposium chairman and editor
Search for other works by this author on:
ISBN-10:
0-8031-0248-8
ISBN:
978-0-8031-0248-4
No. of Pages:
302
Publisher:
ASTM International
Publication date:
1983

The damage tolerance of graphite/epoxy isogrid wide columns in compressive buckling is studied. The observed failure mode in bending was simulated on the panels by cutting grid ribs at nodal sites. The panels were tested nondestructively as clamped wide columns with buckling loads determined by a stiffness plotting technique. Degradation of buckling resistance was determined by progressively damaging lengthwise ribs and retesting the panels. Strains at selected rib sites were measured at each damage level to ascertain the redistribution of stresses. Also, flexual vibration tests were conducted at each damage level to assess the frequency reduction. A finite element analysis provided satisfactory correlation with test data. The results demonstrate that this type of structure is very tolerant to damage.

1.
Meyer
,
R. R.
and
Bellingante
,
R. J.
, “
Fabrication and Experimental Evaluation of Common Domes Having Waffle-Like Stiffening
,” Report Sm-47742,
McDonnell Douglas Astronautics Co.
, Huntington Beach, Calif.,
11
1964
.
2.
Rehfield
,
L. W.
and
Deo
,
R. B.
, “
Continuous Filament Advanced Isogrid Wide Columns in Axial Compression
,” AFOSR TR-79-0021,
U.S. Air Force, Office of Scientific Research, Bolling Air Force Base
,
Washington, D.C.
,
11
1978
.
3.
Reddy
,
A. D.
and
Rehfield
,
L. W.
, “
Behavior of Continuous Filament Isogrid Structure in Bending and Compression
,”
AFOSR report (number to be assigned)
,
U.S. Air Force, Office of Scientific Research, Bolling Air Force Base
, Washington, D.C.,
01
1981
.
4.
Rehfield
,
L. W.
,
Deo
,
R. B.
, and
Renieri
,
G. D.
, “
Continuous Filament Advanced Composite Isogrid: A Promising Structural Concept
,”
Fibrous Composites in Structural Design
,
Plenum Press
,
New York
,
1980
, pp. 215-239.
5.
Rehfield
,
L. W.
and
Reddy
,
A. D.
, “
Damage Tolerance of Continuous Filament Composite Structure: A Preliminary Assessment
,”
Composite Materials: Mechanics, Mechanical Properties, and Fabrication
,
Japan Society for Composite Materials
,
Tokyo
,
1981
, pp. 471-477.
6.
Horton
,
W. H.
,
Cundari
,
F. L.
, and
Johnson
,
R. W.
, “
Applicability of Southwell Plot to the Interpretation of Test Data Obtained from Stability Studies of Elastic Column and Plate Structures
,”
USAAVLABS Technical Report
69-32,
Department of the Army
. Fort Eustis, Va.,
11
1971
.
7.
Jones
,
R. E.
and
Green
,
B. E.
, “
Force/Stiffness Technique for Nondestructive Buckling Testing
,”
Journal of Aircraft
, Vol.
13
, No.
4
,
04
1976
, pp. 262-269.
8.
Bathe
,
K. J.
,
Wilson
,
E. L.
and
Peterson
,
F. E.
, “
Structural Analysis Program for Static and Dynamic Response of Linear Systems
,”
Report EERC
73-11,
University of California
, Berkeley,
06
1973
(revised April 1974).
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