Every nozzle cut into a pressure vessel shell removes metal that was carrying load. ASME VIII Div. 1 handles this with the area replacement method: the metal removed must be put back within defined limits around the opening. This post walks through the method, explains when to use a reinforcing pad, a thicker neck or an insert plate, and works through a complete NPS 6 nozzle example. It builds on our wider guide to pressure vessel and storage tank design . Why an Opening Weakens a Shell A circular hole in a cylindrical shell under internal pressure creates a stress concentration. The peak stress at the edge of a plain hole is roughly 2.5 times the nominal hoop stress, and the hole interrupts exactly the metal that resists hoop stress. For a refresher on how a stress state resolves on different planes, see our note on stress transformation . The Code does not calculate the peak. It requires the removed metal to be replaced close to the opening, which keeps local stresses within the r...
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Stress and Strains
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Stress:
It is defined as force per unit area.
Stress is in direction of force because it is directly proportional to the strain produce which have same direction as that of applied force.
It is a resistance (not a reaction) of material having same direction as that of force.
Stress in Steel Bar > Stress in Rubber Bar ⇔ Because steel have more resistance than rubber.
Ques: Does a rigid body produce stress under the action of load?
No, since there is no relative displacements in rigid body (no change in shape or size). So strain is equal to zero. Since, stress ∝ strain, so stress is equal to zero.
Ques: Is it good to have larger amount of stress produced in material?
No, higher stresses means more chances of failure (fracture). In order to make parts stronger, you need to reduce stress amount produced. For this use stronger material and thicker cross-section.
Types of Stresses:
Normal Stress ⇔ Stress applied perpendicular to cross-section which results in increase or decrease of length.
Shear Stress ⇔ Stress applied parallel to the surface results in angular deformation. It is in opposite direction as that of applied force.
Tensile Stress (+σ) ⇔ Normal Stress applied to elongates a surface.
Compressive Stress (-σ) ⇔Normal Stress applied to compress a surface.
Important Terms:
Prismatic Bar ⇔ Bar having constant cross-section.
Homogenous Bar ⇔ Bar having same composition.
Isotropic Bar ⇔ Bar having same properties in x, y, z directions.
Max. Average Normal Stress ⇔ If bar is subjected to external loads (no constant stress). Hence, stress is present at location where ratio P/A is maximum.
Complementary Property of (Pure) Shear:
Shear stresses having same magnitude but opposite directions are referred to as Complementary Property of Pure Shear.
Single Shear (τ = V/A) ⇔ If load is applied on one plane result in division of 2 parts.
Double Shear (τ = V/2A) ⇔ If load is applied on two plane result in division of 3 parts.
Due to normal or shear stress applied on a structural member, stresses or strains are induced which cause failure. To do the analysis, we divide components into small units showing state of stress.
Each force of cube have one normal and two shear stress.
Ques: Why cube showing state of stress have 1 normal and 2 shear stress on one plane?
If cube is placed on a surface there is only one perpendicular plane, so only one Normal Stress.
If cube is lying on a surface there is only one plane having 2 dimensions parallel to the surface, so two Shear Stresses.
Allowable or Normal Stress:
It is the amount of stress that we permit in material to avoid fracture.
We limit stress to make structural member of mechanical element safe.
To ensure safety, let load be lower than allowable stress and use thicker cross-section.
Ques: What is the value of allowable stress, is it constant?
It cannot be a constant. It depends on load, geometry, supports, orientation and material.
It is defined as, Amount of stress at which material fails (i.e. material before becoming non-functional).
It is a material property.
It describe the strength of material.
Factor of Safety:
It is the ratio of Failure load to the allowable load.
Actual loads is not equal to load we calculate, there are some uncertainties (due to this, stress increase and material fails):
Measurement errors due to the error in fabrication and assembly of components.
No consideration of vibrations, impact and accidental loadings in design.
Strength decreases due to atmospheric corrosion, decay, weather deteriorate occurs.
Wood, concrete, fiber-reinforced composites show variability in mechanical properties.
F.S. in design of aircraft or space vehicle components should be close to 1 to reduce weight.
Larger F.S. means have less chances of failure, thicker, heavier, expensive.
Lesser F.S. means have more chances of failure, thinner, lighter.
Determinacy of System ↣ If number of equations = number of unknowns.
Indeterminacy of System ↣ If number of equations < number of unknowns.
Neutral System ↣ If number of equations > number of unknowns.
Stress Induced in Pressure Vessel:
When pressure is applied, pressure loading comes into play which results in stresses.
Pressure stresses depends on radius of pipe, shape of vessel and pressure applied.
Types of Pressure Vessel:
There are two types of pressure vessel which are discussed ahead:
Thin Wall Pressure Vessel↣ If ratio of inner radius to wall thickness is greater than and equals to 10 (inner radius/wall thickness >= 10)
Thick Wall Pressure Vessel ↣ It does not depend on r/t ratio rather it depends on Elasticity Solution.
1. Thin Wall Pressure Vessel:
There are two types of Thin Wall Pressure Vessel which are discussed ahead:
a. Cylindrical Pressure Vessel:
There are are two types of stresses applied Longitudinal (or Axial) Stresses and Circumferential (or Hoop) Stresses.
a. Spherical Pressure Vessel:
There are are two types of stresses applied Longitudinal (or Axial) Stresses and Circumferential (or Hoop) Stresses and they are equal to each other in case of Spherical Pressure Vessel.
Strain:
It is defined as the Deformation of body under applied stress.
Types of Strains:
Normal Strain ↣ change in length along one specific directions.
Shear Strain↣ change in angle with respect to two specific directions (or deformation perpendicular to original length).
References:
Material from Class Lectures + Book named Engineering Mechanics of Materials by R.C. Hibbeler (10th Edition) + my knowledge.
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