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Main Body (2/6) -- Strength of Materials Supplement for Pow...

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Main Body

Main Body Stress and Strain Stress-Strain Learning Objectives After completing this chapter you should be able to: - Define normal and shear stress and strain and discuss the relationship between design stress, yield stress and ultimate stress - Design members under tension, compression and shear loads - Determine members deformation under tension and compression Tension or compression in a member generate normal stresses; they are called “normal” because the cross-section that resists the load is perpendicular (normal) to the direction of the applied forces. Both tensile and compressive stresses are calculated with: If a member has a variable cross-section, the area that must be used in calculations is the minimum cross-sectional area; this will give you the maximum stress in the member, which ultimately will govern the design. Shear stresses In shear the cross-section area that resists the load is parallel with the direction of applied forces. In addition to that, when estimating the shear area you must factor in how many cross-sections contribute to the overall strength of the assembly. For instance, if you consider the pin of a door hinge as subjected to a shear load, you have to count how many cross-sections resist the load. The formula for calculating the shear stress is the same: In a punching operation the area that resists the shear is in the shape of a cylinder for a round hole (think of a cookie cutter). Therefore the area in shear will be found from multiplying the circumference of the shape by the thickness of the plate. Please note: When looking at textbook figures you will observe that two forces are indicated. This does not mean that the force you use in the formula is (2 × Force P), but simply indicates that one is the Action force and the second one is the Reaction. Normal strain A member in tension or compression will elastically deform proportional with, among other parameters, the original length. Strain, also called unit deformation, is a non-dimensional parameter expressed as: If you choose to use a negative value for compression strain (reduction in length) then you must also express the equivalent compression stress as a negative value. The stress – strain curve is generated from the tensile test. Over the elastic region of the graph the deformation is direct proportional with the load. Dividing the load by the cross-section area (constant) and the deformation by the original length (constant) leads to a graphical representation of Strain vs. Stress. The constant ratio of stress and strain is Young’s Modulus or Elastic Modulus, a property of each material. Combining the above two relations for strain and Modulus of Elasticity leads to a unified formula for elastic deformation in tension or compression. This relation is applicable to members with uniform cross-sections, homogeneous material, subject to tensile or compressive loads that results in stresses below the proportional limit (straight line in the σ-ε curve). These
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