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ASTM Selected Technical Papers
Composite Materials: Testing and Design
By
Steven Yurenka
Steven Yurenka
1
McDonnell Douglas Corp.
, symposium chairman
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ISBN:
978-0-8031-0017-6
No. of Pages:
592
Publisher:
ASTM International
Publication date:
1969
eBook Chapter
Angle-Plied Boron/Epoxy Test Methods—A Comparison of Beam-Tension and Axial Tension Coupon Testing
By
R. B. Lantz
,
R. B. Lantz
1
Senior engineer
, Analytical Section, AVCO Aerostructures Division
, Nashville, Tenn. 37202
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K. G. Baldridge
K. G. Baldridge
2
Supervisor
, Application and Research Laboratory, AVCO Aerostructures Division
, Nashville, Tenn. 37202
. Mr. Baldridge is a personal member ASTM
.
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Page Count:
14
-
Published:1969
Citation
Lantz, RB, & Baldridge, KG. "Angle-Plied Boron/Epoxy Test Methods—A Comparison of Beam-Tension and Axial Tension Coupon Testing." Composite Materials: Testing and Design. Ed. Yurenka, S. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 : ASTM International, 1969.
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A discussion of necessary considerations for tension test specimen design of laminated angle-plied composite materials is presented. Particular attention is paid to the straight-sided axial coupon and the long-beam flexure test. A large amount of test data, including strain gage measurements, has been compiled to provide a basis of comparisons of tensile strengths and elastic properties of angle-plied boron/epoxy laminates by the two test methods.
References
1.
Lenoe
, E. M.
, “Evaluation of Test Techniques for Advanced Composite Materials
,” Quarterly Report No. 5, AVCO Corporation Report AVSSD-0200-68-CR, 1968
.2.
Pagano
, N. J.
and Halpin
. J. C.
, “Influence of End Constraint in the Testing of Anisotropic Bodies
,” Journal of Composite Materials
, Vol. 2
, 1968
, pp. 18–31.3.
Wu
, E. M.
and Thomas
, R. L.
, “Off-Axis Test of a Composite
,” Journal of Composite Materials, Note to the Editor
, Vol. 2
, 1968
, pp. 523–526.4.
“
Application of Advanced Fibrous Reinforced Composite Materials to Airframe Structures
,” Monthly Report No. 5, North American Aviation, Los Angeles Division Report NA-65-993-5, 1966
.5.
Dickerson
, E. O.
and DiMartino
, B.
, “Off-Axis Strength and Testing of Filamentary Materials for Aircraft Application
,” Advanced Fibrous Reinforced Composites, Vol. 10
, 10th National Symposium
, Society of Aerospace Materials and Process Engineers
, 1966
.6.
Waddoups
, M. E.
and Shockey
, P. D.
, Strength and Modulus Determination of Composite Materials with Sandwich Beam Tests
, General Dynamics/Ft. Worth Report FZM 4691, 1966
.7.
“
Advanced Composites Aircraft Application Program-FY 1967 Final Report
,” AVCO Corporation Report R-2020, 1968
.8.
Lantz
, R. B.
, “Effect of Load Angle on the Compressive Failure of Fiberglass/Epoxy Faced, Honeycomb Sandwich Structure
,” AVCO Corporatiori Report R-2031, 1968
.9.
“
Plastics for Flight Vehicles, Part 1, Reinforced Plastics
,” MIL-17, Military Handbook
, 1959
.
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