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naca-tn-1536

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National Advisory Committee for Aeronautics, Technical Notes - Biaxial Plastic Stress Strain Relations for 24S-T Aluminum Alloy

naca-tn-1536-biaxial-plastic-stress-strain-relations-for-24s-t-aluminum-alloy-1

The object of this investigation was to determine the yield m
strength, ultimate strength, ductility, and plastic stress—strain
relations for ens-T aluminum alloy when subjected.to biaxial stresses. >é
Both biaxial stresses considered were tensile and the influence of various
biaxial stress ratios on the mechanical properties was determined.
Biaxial tensile stresses were produced in_a tubular specimen by a
specially_designed testing machine. This testing machine applies both
an axial tensile load and internal pressure to the tubular specimen,
thereby producing biaxial tensile stresses in the tube wall. Strains
were measured in the plastic range up to rupture by means of special
electric SR- 4 clip gages. Nominal stress- strain diagrams for the elastic-w
range and true stress- strain diagrams for the plastic range were plotted
for various biaxial stress ratios. ”—

The data were interpreted by a generalized St. venant theory in an
attempt to predict the biaxial stress— strain relations in terms of the
uniaxial tensile stress- strain relations. The stress- strain relations,
as predicted for combined stresses by this theory agree approximately
with the test results. The yield—strength values, as determined by
tests, agree Quite well with the distortion energy theory, and the
ultimate and fracture strengths agree well with the maximum stress theory._

Stress-strain data were obtained from flat control specimens cut
from the tubular specimens and compared with tension test data obtained
from tubular specimens. Except for ductility values, the results show
that the tension test results for these control specimens agree with the
values for the longitudinal tension tests on the tubular specimens.

Aircraft members may be subjected to stresses beyond the yield
strength of the material. In many cases the stresses are not simple ,,
stresses acting in one direction, but the stresses act in several
directions; that is, the biaxial stresses often occur in place of
uniaxial stresses. It is of importance, therefore, to determine the
plastic stress—strain relations and the mechanical properties in air—
craft materials subjected to coMbined stresses.

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naca-tn-1536

  • Version
  • 159 Downloads
  • 2.28 MB File Size
  • 1 File Count
  • December 4, 2016 Create Date
  • December 4, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Biaxial Plastic Stress Strain Relations for 24S-T Aluminum Alloy

naca-tn-1536-biaxial-plastic-stress-strain-relations-for-24s-t-aluminum-alloy-1

The object of this investigation was to determine the yield m
strength, ultimate strength, ductility, and plastic stress—strain
relations for ens-T aluminum alloy when subjected.to biaxial stresses. >é
Both biaxial stresses considered were tensile and the influence of various
biaxial stress ratios on the mechanical properties was determined.
Biaxial tensile stresses were produced in_a tubular specimen by a
specially_designed testing machine. This testing machine applies both
an axial tensile load and internal pressure to the tubular specimen,
thereby producing biaxial tensile stresses in the tube wall. Strains
were measured in the plastic range up to rupture by means of special
electric SR- 4 clip gages. Nominal stress- strain diagrams for the elastic-w
range and true stress- strain diagrams for the plastic range were plotted
for various biaxial stress ratios. ”—

The data were interpreted by a generalized St. venant theory in an
attempt to predict the biaxial stress— strain relations in terms of the
uniaxial tensile stress- strain relations. The stress- strain relations,
as predicted for combined stresses by this theory agree approximately
with the test results. The yield—strength values, as determined by
tests, agree Quite well with the distortion energy theory, and the
ultimate and fracture strengths agree well with the maximum stress theory._

Stress-strain data were obtained from flat control specimens cut
from the tubular specimens and compared with tension test data obtained
from tubular specimens. Except for ductility values, the results show
that the tension test results for these control specimens agree with the
values for the longitudinal tension tests on the tubular specimens.

Aircraft members may be subjected to stresses beyond the yield
strength of the material. In many cases the stresses are not simple ,,
stresses acting in one direction, but the stresses act in several
directions; that is, the biaxial stresses often occur in place of
uniaxial stresses. It is of importance, therefore, to determine the
plastic stress—strain relations and the mechanical properties in air—
craft materials subjected to coMbined stresses.

FileAction
naca-tn-1536 Biaxial Plastic Stress Strain Relations for 24S-T Aluminum Alloy.pdfDownload 
17,005 Documents in our Technical Library
2727377 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...