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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Viscous Flow In Pipes
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Reynolds Number:
Reynolds Number is the ratio of Inertial forces to the Viscous forces. By knowing this number, one can describe the flow whether the flow is laminar, turbulent or transitional flow.
There are three possibilities of the range of Reynolds Number:
If Reynolds number < 2100 or 2300 ⟺ Laminar Flow
If Reynolds number > 4000 ⟺ Turbulent Flow
If 2300 < Reynolds number < 4000 ⟺ Transitional Flow
In case of different shapes other than circle, the formula for Reynolds Number remain the same however diameter involves in the formula become Hydraulic Diameter which is given by:
For pipe:
Critical Reynolds Number ⟾ The Reynolds number at which the flow becomes turbulent Recr
For different shapes, the hydraulic diameters are given by:
Completely Filled Flow In Closed Channel:
If pipe is is considered to filled completely with closed channel, then following are the conditions which are generated to flow liquid.
If Pressure at 1 < Pressure at 2 ⟼ Flow will be in the direction 1➙2.
If Pressure at 1 = Pressure at 2 ⟼ No flow of liquid, requires external pressure (pump) to flow liquid.
Partially Filled Flow In Open Channel:
If pipe is is considered to filled completely with closed channel, then following are the conditions which are generated to flow liquid.
There is only one condition arises which is:
To flow liquid, pump is required because pressures are equal at any two states because it is open to atmospheric pressure.
Types Of Flow:
There are three types of flow depending upon the behavior of fluid particles which are described as follows:
1. Laminar Flow:
It is characterized by the by smooth streamlines and highly ordered motion. The Reynolds number for Laminar flow is lesser than 2300.
2. Turbulent Flow:
It is characterized by fluctuation in velocity and highly disordered motion. The Reynolds number for Turbulent flow is greater than 4000.
It is the transition from laminar to turbulent flow does not occur suddenly.
Boundary Layer Theory:
When liquid want to flow through a closed or open channel, the layer closes to wall or surface resists due to friction and viscosity which increases with time. The velocity of boundary layer is 0.99 times the free velocity or middle layer velocity.
The Entrance Region:
The length from entrance to the uniform velocity profile is called Hydrodynamic Entry Length. And this region is called Hydrodynamic Entrance Region.
The region after the attainment of uniform velocity profile is called Fully Developed Region.
The hydrodynamic entry length for laminar and turbulent flow are:
Laminar Flow In Pipes:
Consider a ring-shaped differential volume element of radius 'r', thickness 'dr' and length 'dx' oriented co-axially with the pipe. A force balance on the volume element in the flow direction gives:
Pressure & Head Loss For Inclined Pipes:
For inclined pipes, the pressure and head loss is given by introducing sine of θ.
Energy Equation In Terms Of Heads:
Energy equation for calculating various parameters in terms of head is given by:
Where;
Head for Turbine ↔ output energy which we are extracted.
Head Loss ↔ due to decrease in pressure.
Correction Factor, α ↔ it determines the flow is ideal or actual. Its value is in between 0-1.
Turbulent Flow In Pipes:
There are four types of layers which are described as follows:
Viscous (or Laminar or Linear or Wall) Sub-Layer ↣ layer close to wall in which viscous effects are dominant, velocity profile is linear.
Buffer Layer ↣ viscous effects are still dominant but turbulent effects are becoming significant.
Overlap (or Transition) Layer or Inertial Sub-Layer ↣ layer in which turbulent effects are much more significant.
Outer (or Turbulent) Layer ↣ turbulent effects are dominant.
Calculation Of Darcy Friction Factor:
We calculate Darcy Friction Factor by two following ways:
1. By Moody Chart:
To calculate friction factor from moody chart, you should have Reynolds number 'Re' and relative roughness ε/D.
2. By Colebrook Equation:
To calculate Darcy friction factor from Colebrook method, following equation is used.
Minor Losses:
Losses due to elbows or fittings are called Minor Losses. In case of minor losses, a minor loss coefficient or resistance coefficient will appear. Minor losses are given by:
The total head loss is given by:
For number of fittings or elbows, the above equation after summation becomes:
Piping Network:
There are two types of piping network which are discussed ahead:
1. Series Piping System:
The total head loss in the series piping system is equal to the sum of individual head losses and the flow rate remains same.
2. Parallel Piping System:
The total head loss in the series piping system is equal to the sum of flow rate. The pressure drop in each individual pipe connected in parallel are same.
Note: If you want to learn piping system in advance, go and watch it:
References:
Materials From Class Lectures + Own Knowledge + Book named Fundamentals of Fluid Mechanics by Munson, Young and Okiishi's (8th Edition).
What is Sub-critical reynolds nimber? What it matters fluid flow to be laminar or turbulent? Is there any practical application or where this info used?
I am dealing your questions number wise and thanks for showing your interest.
1. First you need to understand Critical Reynolds number and then going towards your question: Critical Reynolds number exists in the transitional region during which flow changes from laminar to turbulent. Sub-critical Reynolds number exits due to fluctuating pressure and skin friction between fluid and surface of geometry through which fluid is flowing. 2. The basic difference between laminar and turbulent flow is turbulency rate. Turbulency is due to skin friction between fluid and surface of geometry through which fluid is flowing, fluctuating pressure or shorter hydrodynamic entrance region. If flow is turbulent, we need more pressure energy to cause fluid to flow. 3. It's applications are very vast. Used when fluid is in contact with moving objects like Airplane, automobiles, wind turbine, vortex phenomena. Hope you'll get your satisfying answer.
TAPING CORRECTIONS There are two types of corrections depending upon the type of errors in tape due to the different conditions. 1. Systematic Errors : Slope Erroneous tape length Temperature Tension Sag 2. Random Errors : Slope Alignment Marking & Plumbing Temperature Tension & Sag 1. Temperature Correction It is necessary to apply this correction, since the length of a tape is increased as its temperature is raised, and consequently, the measured distance is too small. It is given by the formula, C t = 𝛼 (T m – T o )L Where, C t = the correction for temperature, in m. 𝛼 = the coefficient of thermal expansion. T m = the mean temperature during measurement. T o = the tempe...
Center of Gravity: It is defined as; The resultant weight of a system which passes through a single point is called Center of Gravity ( G ). Center of Mass: It is defined as; The point at which the whole mass of the system acts. The concept of center of mass is cleared from the video given below: Centroid of a Volume: Objects having three dimensions have the centroid which is its geometric centre. Centroid of an Area: Objects having two dimensions have the centroid which is its geometric centre. Centroid of a Line: Objects having linear dimensions have the centroid which is its geometric centre. Composite Bodies: A composite body consists of a series of connected simpler shaped Bodies which may be rectangular, triangular, semicircular, etc. References: www.youtube.com www.wikipedia.com http://web.aeromech.usyd.edu.au/statics/doc/friction/Friction1.htm From Book Engineering Mechanics sta...
Moving Boundary Work: The expansion and compression work associated with a piston cylinder device in which boundary moves is called Moving Boundary Work. Area under the Process curve on a PV Diagram: From the above figure, the differential area is the product of pressure and differential volume. So the area under the Process curve is given by: The area under the Process cure on a PV Diagram is Moving Boundary Work. Moving Boundary Work in A constant Volume Process: Moving boundary work is given by: Moving Boundary Work for a Constant Pressure Process: Moving Boundary Work is given by: Moving Boundary Work for an Isothermal Process: A thermodynamic process in which temperature remains constant durine the heat transfer is called Isothermal Process. Moving Boundary Work is given by: Where; PV = mRT If temperature is constant,then PV = c P = c/V Moving Boundary Work for P...
What is Sub-critical reynolds nimber? What it matters fluid flow to be laminar or turbulent? Is there any practical application or where this info used?
ReplyDeleteI am dealing your questions number wise and thanks for showing your interest.
Delete1. First you need to understand Critical Reynolds number and then going towards your question: Critical Reynolds number exists in the transitional region during which flow changes from laminar to turbulent. Sub-critical Reynolds number exits due to fluctuating pressure and skin friction between fluid and surface of geometry through which fluid is flowing.
2. The basic difference between laminar and turbulent flow is turbulency rate. Turbulency is due to skin friction between fluid and surface of geometry through which fluid is flowing, fluctuating pressure or shorter hydrodynamic entrance region. If flow is turbulent, we need more pressure energy to cause fluid to flow.
3. It's applications are very vast. Used when fluid is in contact with moving objects like Airplane, automobiles, wind turbine, vortex phenomena.
Hope you'll get your satisfying answer.