Composite Materials Questions and Answers – Static Mechanical Properties

This set of Composite Materials Multiple Choice Questions & Answers (MCQs) focuses on “Static Mechanical Properties”.

1. Which static test is used to determine the tensile properties of flat composite laminates?
a) ASTM D7264
b) ASTM D3039
c) ASTM D3518
d) ASTM D4236
View Answer

Answer: b
Explanation: Tensile properties such as tensile modulus, tensile strength and Poisson’s ratio of flat composite laminates are determined using standard test method ASTM D3039. Straight-sided tensile specimens having constant cross-section are generally used for this test.

2. The end tabs in a tensile test specimen are made of a compliant and strain-compatible material.
a) True
b) False
View Answer

Answer: a
Explanation: The end tabs are adhesively bonded to the ends of the tensile specimen. The strain-compatible material is used at the end tabs in order to reduce the stress concentrations in the gripped area. It promotes tensile failure in the gage sections.

3. The tensile specimen is held in a testing machine by plane grips.
a) True
b) False
View Answer

Answer: b
Explanation: In tensile testing, the specimen is held by wedge action grips. The specimen is pulled at a recommended cross-head speed of 2 mm/min.
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4. Which device is used to measure the different strains in a tensile testing specimen?
a) Electrical resistance strain gauges
b) Mechanical strain gauges
c) Optical strain gauges
d) Pneumatic strain gauges
View Answer

Answer: a
Explanation: An Electrical resistance strain gauge is used to measure the longitudinal and transverse strains in a tensile testing specimen. The device is bonded in the gage section of the specimen.

5. A tensile load creates both extension and shear deformations for an off-axis unidirectional specimen.
a) True
b) False
View Answer

Answer: a
Explanation: In an off-axis unidirectional specimen, the tensile load induces shear forces and bending couples, the specimen ends are constrained by the grips that create non-uniform S-shaped deformation in the specimen since its ends are constrained by the grips.

6. What causes the failure of unidirectional laminate specimens?
a) Interfacial shear failure
b) Matrix tensile rupture
c) Matrix shear failure
d) Longitudinal splitting
View Answer

Answer: d
Explanation: In the unidirectional laminates, the specimen fails by the longitudinal splitting parallel to the fibers. Longitudinal splitting is the de-bonding along the fiber-matrix interface which gives a typical broom-like appearance in the failed area of the specimens.

7. For off-axis specimens, the failure may occur by fiber-matrix shear failure.
a) True
b) False
View Answer

Answer: a
Explanation: The failure in off-axis specimens may occur by fiber-matrix interfacial shear failure, matrix tensile rupture and matrix shear failure. For these specimens, the tensile stress-strain curve may exhibit non-linearity.
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8. Which fiber orientation angle of the laminas shows the maximum tensile modulus?
a) At θ=0°
b) At θ=30°
c) At θ=45°
d) At θ=90°
View Answer

Answer: a
Explanation: The tensile modulus and strength of a unidirectional specimen depends greatly on the fiber orientation angle(θ). The magnitude of these properties decreases with increasing fiber orientation angle. The minimum values of tensile strength and modulus are observed near 90° fiber orientation angle.

9. The fibers in a multidirectional laminate are in different fiber orientations.
a) True
b) False
View Answer

Answer: a
Explanation: The Tensile stress-strain curves for multidirectional laminates containing different fiber orientations are in nonlinear. A number of knee points are also observed in the stress-strain curve. The knee point is the point at which the two linear sections intersects.
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10. What is the first knee point in a tensile stress-strain diagram?
a) First Knee Failure point
b) First Ply Failure point
c) First Fracture Failure point
d) Initial Knee Failure point
View Answer

Answer: b
Explanation: First Ply Failure (FPF) point has a great importance in laminate designs. For the laminates having high notch sensitivity, the failure occurs just after the First Ply Failure point. The cracks occurring at the FPF will lead to the possibility of fatigue failure as well as environmental damage.

Sanfoundry Global Education & Learning Series – Composite Materials.

To practice all areas of Composite Materials, here is complete set of 1000+ Multiple Choice Questions and Answers.

If you find a mistake in question / option / answer, kindly take a screenshot and email to [email protected]

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Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

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