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please in a clear answer find me those and use table for
(Epoxy):
the yield stress...
please in a clear answer find me those and using the table for (polyprolene): the yield...
please in a clear answer find me those and using the table for
(polyprolene):
the yield stress
the ultimate tensile stress(uts)
breaking strain
Dimension of Polymer Samples Sample Name Polyethylene Polypropylene Epoxy Rubber Width(mm) 12 12 12 4 Thickness (mm) 3 3 5 2 Gauge length (mm) 42 42 42 14 C/Users/alkha/Downloads/Experiment%201.pdf Load (N) Polypropylene (thermoplastic) 1500 1000 Bro 500 00 0.0 60 150 20.0 10.0 Machine Extension (mm)
please in a clear answer find me those and using the table for (polyethlene): the yield...
please in a clear answer find me those and using the table for
(polyethlene):
the yield stress
the ultimate tensile stress(uts)
breaking strain
Dimension of Polymer Samples Sample Name Polyethylene Polypropylene Epoxy Rubber Width(mm) 12 12 12 4 Thickness (mm) 3 3 5 2 Gauge length (mm) 42 42 42 14 w You X Pos X 6 px Q (68) X e Ten: X 0 im x (68 X SAFX in File C/Users/alkha/Downloads/Experiment%201.pdf Load (N) Polyethylene (thermoplastic) 1000 900 800...
please in a clear answer find me those: the yield stress the ultimate tensile stress(uts) breaking...
please in a clear answer find me those:
the yield stress
the ultimate tensile stress(uts)
breaking strain
50.30 11.15 6.00 26.00 R1.00 0 11.00 R1.50 04.00 07.14 Load (N) Tool Steel 25000 Break 20000 15000 10000 5000 000 3.0 40 00 20 Machine Extension (mm)
please in a clear answer find me those: the yield stress the ultimate tensile stress(uts) breaking...
please in a clear answer find me those:
the yield stress
the ultimate tensile stress(uts)
breaking strain
37.20 5.00 25.20 + R1.00 File c/Users/alkha/Downloads/Experiment%201.pdf Load (N) Low Carbon Steel 15000 10000 5000 000 00 10 5.0 30 Machine Extension (mm)
this is a lab please provide me with clear answeres and measure : - yeild stress...
this is a lab
please provide me with clear answeres and measure :
- yeild stress
- ultimate tensile stress
-breaking strain
-young's modulus
52.70 7.00 35.70 R1.50 00'ιιο Φ7.14 Load (N) Aluminium 6000 5000 4000 3000 2000 1000 000 100 50 Machine Extension (mm)
These graphs are stress vs strain curves for each metal and polymer samples. Label the graphs...
These graphs are stress vs strain curves for each metal and
polymer samples. Label the graphs where the material showed UTS,
yield stress and beraking strain.
7000 4000 3000 Break 1000 0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 Machine Extension (mm)
I have a question during my Tensile Test of Sturctural Steel. Ive collected all the data, can you calculate the Elastic...
I have a question during my Tensile Test of Sturctural
Steel.
Ive collected all the data, can you calculate the Elastic
Modulus and referring to the stress strain curve of your samples ,
discuss and compare the results, specify the similarities and
differences if there is any and provide possible reasons.
Thanks
Date of Lab Mark (for tutor only) 1. General information of the sample: Web sample or flange sample? web Specimen dimension (Before Testing) Width, mm Gauge length, mm...
5. EVALUATION I. Create a stress-strain diagram for the measured values in table 1 and identify...
5. EVALUATION I. Create a stress-strain diagram for the measured values in table 1 and identify the mechanical properties of the material. (4 marks) II. Identify the following and label them in the graph. (12 marks) • Young's modulus Yield strength Elongation Ultimate tensile strength THEORETICAL BACKGROUND Equations: Cross-sectional Area (A) Modulus of Elasticity (E) Tensile Strength (ST) Percent Elongation (%EL) d? E = Sy Ey Sr Pu А %EL Extension at fracture Gauge Length Where: A: Cross- Sectional Area...
Please provide me clear handwriting Table 1: TENSILE TEST RESULTS OF A METAL SAMPLE with d...
Please provide me clear handwriting
Table 1: TENSILE TEST RESULTS OF A METAL SAMPLE with d = 7.42, lo = 40mm (4 marks) Load, KN Extension, mm Stress, MPa Strain 0 0 10 0.05 17 0.08 25 0.11 30 0.14 34 0.20 37.5 0.40 38.5 0.60 36 0.90 Cross-sectional Area (A) Modulus of Elasticity (E) Tensile Strength (ST) Percent Elongation (%EL) A = T d2 4 E = Sy Ey ST = PU A %EL = Extension at fracture Gauge...
235 Find the off-axis shear strength and mode of failure of a 60 boron/ epoxy lamina. Use the pro...
235 Find the off-axis shear strength and mode of failure of a 60 boron/ epoxy lamina. Use the properties of a unidirectional boron/epoxy lamina from Table 2.1. Apply the maximum stress failure, maximum strain, Tsai-Hill, and Tsai-Wu failure theories. TABLE 2.1 Tvpical Mechanical Properties of a Unidirectional Lamina (SI System of Units) Glass Boron/ Graphite/ Property SymbolUnits epoxy epoxy epoxy Fiber volume fraction Longitudinal elastic modulus Transverse elastic modulus Major Poisson's ratio Shear modulus Ultimate longitudinal tensile strength Ultimate longitudinal...
please in a clear answer find me those and using the table for
(polyprolene):
the yield stress
the ultimate tensile stress(uts)
breaking strain
Dimension of Polymer Samples Sample Name Polyethylene Polypropylene Epoxy Rubber Width(mm) 12 12 12 4 Thickness (mm) 3 3 5 2 Gauge length (mm) 42 42 42 14 C/Users/alkha/Downloads/Experiment%201.pdf Load (N) Polypropylene (thermoplastic) 1500 1000 Bro 500 00 0.0 60 150 20.0 10.0 Machine Extension (mm)
please in a clear answer find me those and using the table for
(polyethlene):
the yield stress
the ultimate tensile stress(uts)
breaking strain
Dimension of Polymer Samples Sample Name Polyethylene Polypropylene Epoxy Rubber Width(mm) 12 12 12 4 Thickness (mm) 3 3 5 2 Gauge length (mm) 42 42 42 14 w You X Pos X 6 px Q (68) X e Ten: X 0 im x (68 X SAFX in File C/Users/alkha/Downloads/Experiment%201.pdf Load (N) Polyethylene (thermoplastic) 1000 900 800...
please in a clear answer find me those:
the yield stress
the ultimate tensile stress(uts)
breaking strain
50.30 11.15 6.00 26.00 R1.00 0 11.00 R1.50 04.00 07.14 Load (N) Tool Steel 25000 Break 20000 15000 10000 5000 000 3.0 40 00 20 Machine Extension (mm)
please in a clear answer find me those:
the yield stress
the ultimate tensile stress(uts)
breaking strain
37.20 5.00 25.20 + R1.00 File c/Users/alkha/Downloads/Experiment%201.pdf Load (N) Low Carbon Steel 15000 10000 5000 000 00 10 5.0 30 Machine Extension (mm)
this is a lab
please provide me with clear answeres and measure :
- yeild stress
- ultimate tensile stress
-breaking strain
-young's modulus
52.70 7.00 35.70 R1.50 00'ιιο Φ7.14 Load (N) Aluminium 6000 5000 4000 3000 2000 1000 000 100 50 Machine Extension (mm)
These graphs are stress vs strain curves for each metal and
polymer samples. Label the graphs where the material showed UTS,
yield stress and beraking strain.
7000 4000 3000 Break 1000 0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 Machine Extension (mm)
I have a question during my Tensile Test of Sturctural
Steel.
Ive collected all the data, can you calculate the Elastic
Modulus and referring to the stress strain curve of your samples ,
discuss and compare the results, specify the similarities and
differences if there is any and provide possible reasons.
Thanks
Date of Lab Mark (for tutor only) 1. General information of the sample: Web sample or flange sample? web Specimen dimension (Before Testing) Width, mm Gauge length, mm...
5. EVALUATION I. Create a stress-strain diagram for the measured values in table 1 and identify the mechanical properties of the material. (4 marks) II. Identify the following and label them in the graph. (12 marks) • Young's modulus Yield strength Elongation Ultimate tensile strength THEORETICAL BACKGROUND Equations: Cross-sectional Area (A) Modulus of Elasticity (E) Tensile Strength (ST) Percent Elongation (%EL) d? E = Sy Ey Sr Pu А %EL Extension at fracture Gauge Length Where: A: Cross- Sectional Area...
Please provide me clear handwriting
Table 1: TENSILE TEST RESULTS OF A METAL SAMPLE with d = 7.42, lo = 40mm (4 marks) Load, KN Extension, mm Stress, MPa Strain 0 0 10 0.05 17 0.08 25 0.11 30 0.14 34 0.20 37.5 0.40 38.5 0.60 36 0.90 Cross-sectional Area (A) Modulus of Elasticity (E) Tensile Strength (ST) Percent Elongation (%EL) A = T d2 4 E = Sy Ey ST = PU A %EL = Extension at fracture Gauge...
235 Find the off-axis shear strength and mode of failure of a 60 boron/ epoxy lamina. Use the properties of a unidirectional boron/epoxy lamina from Table 2.1. Apply the maximum stress failure, maximum strain, Tsai-Hill, and Tsai-Wu failure theories. TABLE 2.1 Tvpical Mechanical Properties of a Unidirectional Lamina (SI System of Units) Glass Boron/ Graphite/ Property SymbolUnits epoxy epoxy epoxy Fiber volume fraction Longitudinal elastic modulus Transverse elastic modulus Major Poisson's ratio Shear modulus Ultimate longitudinal tensile strength Ultimate longitudinal...
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