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ASTM Selected Technical Papers
Joining of Composite Materials
By
KT Kedward
KT Kedward
1
Materials Sciences Corp.
,
El Cajon, Calif. 92021
;
symposium chairman and editor
.
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ISBN-10:
0-8031-0699-8
ISBN:
978-0-8031-0699-4
No. of Pages:
197
Publisher:
ASTM International
Publication date:
1981

Results of a design data development program involving hundreds of graphite epoxy bolted joint tests are summarized. Emphasis was on obtaining information for HMF330C/34 cloth material at room temperature, 394, and 450 K; however, many specimens made from T300/5208 and AS/3501 tape laminates were tested to provide correlating information on bearing behavior and the importance of hole-bolt tolerances. Bearing strengths for quasi-isotropic laminates made from these three prepregs were similar. Complete removal of bolt torque was shown to reduce the bearing strength relative to fully torqued bolts by approximately 40 percent. Multiple bolt joints were tested using three different hole-bolt tolerances. Resulting strengths were encouragingly similar, indicating the materials were less brittle than might have been expected. This was particularly true for bearing failures. Loaded-bolt and open-hole tests on cloth laminates indicated a greater degree of effective ductility than indicated by available data for similar tape laminates. Layups with no 45-deg plies exhibited markedly greater brittleness than their quasi-isotropic brethren. The higher the temperature, the less was the ductility for both layups. Bolt head details were shown to exercise a strong influence on bearing strength for single lap joints.

1.
Waszczak
,
J. P.
and
Cruse
,
T. A.
, “
Failure Mode and Strength Predictions of Anisotropic Bolt Bearing Specimens
,” Paper 71-354 in
Proceedings
,
Twelfth Structures, Dynamics, and Materials Conference
,
Anaheim, Calif.
,
04
1971
.
2.
Hadcock
,
R. M.
,
Corvelli
,
N.
, and
Torczyner
,
R. D.
, “
Joints in Composite Structures
,”
Proceedings
,
Second Conference on Fibrous Composites in Flight Vehicle Design
,
Dayton, Ohio
, AFFDL-TR-72-130,
Air Force Flight Dynamics Laboratory
,
09
1972
, pp. 793.
3.
Van Siclen
,
R. C.
, “
Evaluation of Bolted Joints in Graphite/Epoxy
,”
Proceedings
,
Army Symposium—Structural Joints
, AMMRC MS 74-8,
Army Materials and Mechanics Research Center
,
09
1974
, pp. 120-138.
4.
Oplinger
,
D. W.
and
Gandhi
,
K. R.
, “
Analytical Studies of Structural Performance in Mechanically Fastened Fiber Reinforced Plates
,”
Proceedings
,
Army Symposium—Structural Joints
, AMMRC MS 74-8,
Army Materials and Mechanics Research Center
,
09
1974
, pp. 211-241.
5.
Eisenman
,
J. R.
, “
Bolted Joint Static Strength Model for Composite Materials
,”
Proceedings
,
Third Conference on Fibrous Composites in Flight Vehicle Design
, NASA TMX 3377,
National Aeronautics and Space Administration
,
1975
, pp. 563-602.
6.
Collings
,
T. A.
, “
The Strength of Bolted Joints in Multi-Directional CFRP Laminates
,”
Composites Journal
,
01
1977
, pp. 43-55.
7.
Hart-Smith
,
L. J.
, “
Bolted Joints in Graphite/Epoxy Composites
,” NASA CR-144899,
National Aeronautics and Space Administration
,
06
1976
.
8.
Hart-Smith
,
L. J.
in
Fibrous Composites in Structural Design
,
Lenoe
,
E. M.
,
Oplinger
,
D. W.
, and
Burke
,
J. J.
, Ed.,
Plenum
,
New York
,
1980
, pp. 543-574.
9.
Whitman
,
B.
,
Shyprykevich
,
P.
, and
Whiteside
,
J.
, “
Design of the B-1 Composite Horizontal Stabilizer Root Joint
,”
Proceedings
,
Third Conference on Fibrous Composites in Flight Vehicle Design
, NASA TM 3377,
National Aeronautics and Space Administration
,
1975
, pp. 603-631.
10.
Garbo
,
S. P.
and
Ogonowski
,
J. M.
, “
Effect of Variances and Manufacturing Tolerances on the Design Strength and Life of Mechanically Fastened Composite Joints
,” AFFDL-TR-78-179,
Air Force Flight Dynamics Laboratory
,
12
1978
.
11.
Verette
,
R. M.
and
Labor
,
J. D.
, “
Structural Criteria for Advanced Composites
,” AFFDL-TR-76-142,
Air Force Flight Dynamics Laboratory
,
03
1977
.
12.
Agarwal
,
B. L.
, “
Static Strength Prediction of Bolted Joints in Composite Materials
,”
Proceedings
,
20th Structures, Dynamics, and Materials Conference
,
St. Louis, Mo.
,
03
1979
.
13.
Ramkumar
,
R. L.
, “
Bolted Joint Design
,”
Proceedings
,
American Society for Testing and Materials Symposium on Test Methods and Design Allowables for Fibrous Composites
.
Dearborn, Mich.
, Oct. 3rd and 4th, 1979.
14.
Wichorek
,
G. R.
in
Graphite/Polyimide Composites
, NASA CP 2079,
National Aeronautics and Space Administration
,
03
1979
, pp. 249-258.
15.
Wilkins
,
D. J.
in
Composite Materials: Testing and Design (Fourth Conference)
, ASTM STP 617,
American Society for Testing and Materials
,
1977
, pp. 497-513.
16.
Garbo
,
S. P.
and
Ogonowski
,
J. M.
, “
Strength Predictions of Composite Laminates with Unloaded Fastener Holes
,”
Proceedings
,
20th Structures, Dynamics, and Materials Conference
,
St. Louis, Mo.
,
03
1979
, pp. 310-314.
17.
Hyer
,
M. W.
and
Lightfoot
,
M. C.
, “
Composite Bolted-Joint Specimens: Experimental Results
,” NASA CR 158964,
National Aeronautics and Space Administration
,
12
1978
.
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