1.1 Introduction
In an earlier book in this series, The Effect of Temperature and Other Factors on Plastics and Elastomers,1 the general mechanical properties of plastics were discussed. These mechanical properties as a function of temperature, humidity, and other factors are presented in graphs or tables. That work includes hundreds of graphs of stress versus strain, modulus versus temperature, impact strength versus temperature, etc. However, when one starts designing products made of plastics, these graphs do not supply all the necessary information. This is because these graphs show the results of relatively short-term tests. Their value in design is in the initial selection of materials in terms of stiffness, strength, etc. Designs based on short-term data obtained from a short-term test would not predict accurately the long-term behavior of plastics. This is partly because plastics are viscoelastic materials. Viscoelastic by definition means possessing properties that are both solid-like and liquid-like. More precisely with reference to plastics, viscoelastic means that measurements such as modulus, impact strength, and coefficient of friction are sensitive not only to straining rate, temperature, humidity, etc., but also to elapsed time and loading history. The manufacturing method used for the plastic product can also create changes in the structure of the material, which have a pronounced effect on properties.
The rest of this chapter first deals with the types of stress and provides a short introduction to creep. Then the chemistry of plastics is discussed and because plastics are polymeric materials the focus is more on polymer chemistry. The discussion includes polymerization chemistry and the different types of polymers and how they differ from each other. As plastics are rarely “neat,” reinforcements, fillers, and additives are reviewed. This is followed by a detailed look at creep, including creep-specific tests and creep graphs. The discussion takes a look at what happens at the microscopic level when plastics exhibit creep. Section 1.4. is taken from The Effect of Temperature and Other Factors on Plastics and Elastomers book, but it has been refocused on creep properties.
1.2 Types of Stress
Creep is the time-dependent change in the dimensions of a plastic article when it is subjected to a constant stress. Stress can be applied in a number of ways. Normal stress (σ) is the ratio of the applied force (F) over the cross-sectional area (A), as shown in Equation 1.1:
1.2.1 Tensile and Compressive Stress
When the applied force is directed away from the part, as shown in Fig. 1.1, it is a tensile force inducing a tensile stress. When the force is applied towards the part, it is a compressive force inducing a compressive stress.
Figure 1.1. Illustration of tensile stress and compressive stress.
1.2.2 Shear Stress
Shear stress (τ) is also expressed as the force per unit area, as shown in Equation 1.2. The shear force is applied parallel to the cross-sectional area “A” as shown in Fig. 1.2.
Figure 1.2. Illustration of shear stress.
1.2.3 Torsional Stress
Torsional stress (τ) occurs when a part such as a rod or shaft is twisted as in Fig. 1.3. This is also a shear stress, but the stress is variable and depends on how far the point of interest is from the center of the shaft. The equation describing this stress is shown in Equation 1.3:
Figure 1.3. Illustration of torsional stress.
In this equation, T is the torque and c is the distance from the center of the shaft or rod. K is a torsional constant that depends on the geometry of the shaft, rod, or beam. The torque (T) is further defined by Equation 1.4, in which θ is the angle of twist, G is the modulus of rigidity (material dependent), and L is the length.
The torsional constant (K) is dependent upon geometry, and the formulas for several geometries are shown in Fig. 1.4. Additional formulas for the torsional constant have been published.2
Figure 1.4. Torsional constants for rods or beams of common geometries.
1.2.4 Flexural or Bending Stress
Bending stress or flexural stress commonly occurs in two instances, as shown in Fig. 1.5. One is called a simple, supported structural beam bending and the other is called cantilever beam bending. For the simple, supported structural beam, the upper surface of the bending beam is in compression and the bottom surface is in tension. The neutral axis (NA) is a region of zero stress. The bending stress (σ) is defined by Equation 1.5, where M is the bending moment (which is calculated by multiplying a force by the distance between the point of interest and the force), c is the distance from the neutral axis (NA in Fig. 1.5), and I is the moment of inertia. The cantilevered beam configuration, which is also shown in Fig. 1.5, has a similar formula. The formulas for M, c, and I can be complex, depending on the exact configuration and beam shape, but many have been published.3
Figure 1.5. Illustration of flexural or bending stress.
1.2.5 Hoop Stress
Hoop stress (σh) is the mechanical stress defined for rotationally symmetric objects such as pipe or tubing. The real world view of hoop stress is the tension applied to the iron bands, or hoops, of a wooden barrel. It is the result of forces acting circumferentially. Figure 1.6 shows stresses caused by the pressure (P) inside a cylindrical vessel. The hoop stress is indicated on the right in Fig. 1.6, which shows a segment of the pipe.
Figure 1.6. Illustration of hoop stress.
The classic equation for hoop stress created by an internal pressure on a thin-wall cylindrical pressure vessel is given in Equation 1.6:
where P is the internal pressure, t is the wall thickness, and r is the radius of the cylinder. The SI unit for P is pascal (Pa), while t and r are in meters (m).
If the pipe is closed at the ends, any force applied on them by the internal pressure will induce an axial or longitudinal stress (σ1) on the same pipe wall. The longitudinal stress, under the same conditions as in Fig. 1.6, is given by Equation 1.7:
There could also be a radial stress especially when the pipe walls are thick, but thin-walled sections often have negligibly small radial stress (σr). The stress in the radial direction at a point in the tube or cylinder wall is shown in Equation 1.8:
where P is the internal pressure in the tube or cylinder, a is the internal radius of the tube or cylinder, b is the external radius of the tube or cylinder, and r is the radius to the point in tube where the radial stress is calculated.
Often the stresses in a pipe are combined into a measure called the equivalent stress, which is determined using the Von Mises equivalent stress formula shown in Equation 1.9:
where σ1 is the longitudinal stress, σh is the hoop stress, and τc is the tangential shear stress (from material flowing through the pipe).
Failure by fracture in cylindrical vessels is dominated by hoop stress in the absence of other external loads because it is the largest principal stress...