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Page Title: Types of Applied Stress
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Types of Stress
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Material Science Volume 1 of 2
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Tensile Stress

Properties of Metals DOE-HDBK-1017/1-93 STRESS Pressure stresses are stresses induced in vessels containing pressurized materials.  The loading is provided by the same force producing the pressure.  In a reactor facility, the reactor vessel is a prime example of a pressure vessel. Flow  stresses  occur  when  a  mass  of  flowing  fluid  induces  a  dynamic  pressure  on  a conduit wall.   The force of the fluid striking the wall acts as  the load.   This type of stress may be applied in an unsteady fashion when flow rates fluctuate.  Water hammer is an example of a transient flow stress. Thermal   stresses   exist  whenever  temperature  gradients  are  present  in  a  material. Different temperatures  produce  different expansions  and subject materials  to  internal stress.   This type of stress is particularly noticeable in mechanisms operating at high temperatures  that  are  cooled  by  a  cold  fluid.   Thermal  stress  is  further  discussed  in Module 3. Fatigue stresses are due to cyclic application of a stress.   The stresses could be due to vibration or thermal cycling.   Fatigue stresses are further discussed in Module 4. The  importance  of  all  stresses  is  increased  when  the  materials  supporting  them  are  flawed. Flaws tend to add additional stress to a material.   Also, when loadings are cyclic or unsteady, stresses can effect a material more severely.  The additional stresses associated with flaws and cyclic loading may exceed the stress necessary for a material to fail. Stress  intensity within the body of a component is  expressed as  one  of three basic types  of internal  load.   They  are  known  as  tensile,  compressive,  and  shear.   Figure  1  illustrates  the different types  of stress.   Mathematically, there  are only two types  of internal  load because tensile and compressive stress  may be regarded as  the positive and negative versions  of the same type of normal loading. Rev. 0 Page 3 MS-02

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