View Factor Orientation (or View factor or shape factor) plays an important role in radiation heat transfer. View factor is defined as, "fraction of radiation leaving surface 'i' and strike 'j' ". Summation Rule (View Factor) If there is are similar surfaces 'i' and 'j' , then: Blackbody Radiation Exchange Radiation Exchange between Opaque, Diffuse, Gray surfaces in an Enclosure 1. Opaque 2. Surfaces 3. Two surface enclosure Radiation Shield It is used to protect surfaces from radiation act like a reflective surface. References: Material from Class Lectures + Book named Fundamentals of Heat and Mass Transfer by Theodore L. Bergman + My knowledge. Photoshoped pics are developed. Some pics and GIF from Google. Videos from YouTube ( Engineering Sights ).
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Equilibrium of a Particle and Force System Resultants
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Equilibrium of a Particle
Equilibrium:
A particle is said to be in equilibrium if it remains at rest or moving with constant velocity and does not rotate about any axis.
This condition of rest or moving with constant velocity is also called Static Equilibrium.
Coplanar Force Systems:
If a particle is subjected to a system of coplanar forces that lie in the x-y plane then every forces can be resolved into its components.
Since, it is 2D so the equilibrium equations are:
Σ Fx = 0
Σ Fy = 0
3D Force System:
In case of three-dimensional force system, we can resolve the forces into their respective rectangular components.
So the equations of equilibrium are:
Σ Fx = 0
Σ Fy = 0
Σ Fz = 0
Force System Resultants
When a force is applied to a body it will produce a tendency of rotation of body about a point which us not on the line of action of force.
Moment of a Force (Scalar Formulation):
In this sense, the momen is considered as scalar and us calculated as:
Moment = (Force) × (Moment Arm)
M = Fd
Cross Product Formulation of Moment of A Force:
The moment of a force will be formulated using Cartesian vectors is given by:
Principle of Moment:
Principle of moment or Varignon's Theorem states that:
The moment of a force about a point is equal to the sum of the moments of the components of the force about that point.
This method is generally easier than finding the same moment using M = Fd.
Moment of a Force about a Specified Axis:
To determine the turning effect of a force, we can use scalar or vector analysis.
1. Scalar Analysis:
By using the scalar analysis of Turning effect of a force, we have:
M = Fd
2. Vector Analysis:
The vector analysis of moment of a force about an axis is given by:
Couple:
It is defined as:
Two parallel forces that have the same magnitude bit opposite directions and are separated by a distance (d).
Moment of Couple:
The moment produced by a couple is called Moment of a Couple.
We determine the moment of Couple of a system by the algebraic sum of moments acted on the object, which is given by:
M = Ma + Mb
Couple moment is a free vector, so it only depends on the position vector between the forces.
There are two analysis of formulating couple moment:
1. Scalar Formulation:
The moment of Couple by using scalar Formulation is given by :
M = Fd
2. Vector Formulation:
The moment of Couple by using vector Formulation is given by:
M = r × FΣ
Equivalent Couples:
If two couples produce a moment with the same magnitude and direction, then these two couples are equivalent.
Resultant Couple Moment:
Since, couple moments are vectors, their resultant can be determined by vector addition.
M = Σ(r × F)
Or
Resultant Force = ΣF
Resultant Moment = ΣM at origin + ΣM
Or
Resultant Force along x = ΣFx
Resultant Force along y = ΣFy
Resultant Moment at O = ΣMo + ΣM
Reduction of a Simple Distributed Loading:
A uniformly distributed load is a load that is distributed or spread across the whole region of an element. In other words, the magnitude of the load remains uniform throughout the whole element.
Magnitude of Resultant Force:
The Magnitude of resultant force Fr is equivalent to the sum of all the forces in the system, which is given by:
Location of Resultant Force:
The location of force or the geometric center or centroid of the area under the distributed loading is given by:
And, the location of centroid of area under distributive loading for different shapes are:
Solid Mechanics OR Mechanics of Materials OR Strength of Materials: It is the study of mechanics of body i.e. forces and their effects on deformable solids under different loading conditions. Deformable Body Mechanics: It is the study of non-rigid solid structures which deform under load. Deformation/Distortion ⇾ change of shape and size OR have some relative displacement or rotation of particles. It happens when we apply combined load. Rigid Body Motion ⇾ Translation or rotation of particles but having constant distance between particles. Since deformation occur at particular load. Below this load, every body is considered as rigid body . Types of Load: Point Load ⇾ Load apply on a single point i.e. concentrated load. Uniformly Distributed Load (UDL) ⇾ Load remains uniform throughout an area of element like beam. Varying Distributed Load (VDL) ⇾ Load varies with length with constant rate. Moment ⇾ It measures the tend...
Types Of Lines And Its Uses: There are three types of types on the basis of thickness and they are: Visible Lines ↝ It represents features that can be seen in the current view. Hidden Lines ↝ It represents features that cannot be seen in the current view. Center Line ↝ It represents symmetry, path of motion, centers of circles,, axis of asymmetrical parts. Dimension and Extension Lines ↝ It indicates the sizes and location of features on a drawing. Placement Of Dimension Lines: Dimension should be outside the view. Dimension should be applied to one view. Dimension should be placed in a view that shows the distance in its true length. Dimension lines should be placed, in general 10 mm (1/2 in) away from the outlines from the view. Parallel lines should be placed uniformly. Values should be midway (auto centered) between the arrow heads, except when a center-line interferes. Dime...
Introduction To Structural OR Concrete Design Beams must have adequate strength against different types of failure which are: Shear more dangerous than Flexural (or Bending) failure because it creates additional tensile stresses. E.g.: Airplane wing (act as cantilever beam ) and made of Nanocomposites, composites, aluminum. Following are the types of failures in Beam: Flexural (or bending) failure Diagonal Tension failure Shear-Tension failure Shear-Compression failure Following are the types of Shear : Longitudinal Shear Transverse Shear Shear Failure Diagonal Tension Failure ↠ Shear failure of reinforced concrete beam (difficult to predict). Only valid for Homogenous beams . When we apply load on beam ↠ Bending as well as Shear stresses are produced. Shear stress have maximum value at Neutral axis N.A. Bending stress have maximum value at Extreme fibers. At maximum bending stress ↠ shear stress = 0 . Assumptions for shear stresses i...
You can better get Engineering statics material from YouTube by the same name engineering statics
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