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.
Rankine Cycle Rankine cycle is an ideal cycle for Vapour Power Cycles and is normally used for Electricity Generation. The Rankine cycle consist of following steps: 1 ↝ 2 : Isentropic Compression in Pump. 2 ↝ 3 : Constant Pressure Heat Addition in Boiler. 3 ↝ 4 : IsentropicExpansion in Turbine. 4 ↝ 1 : Constant Pressure Heat Rejection in Condenser. Energy Balance: Since, all the devices which Rankine Cycle posses are steady flow devices, so the energy balance for Rankine cycle is: 》For Pump ( q = 0 ): 》For Boiler ( w = 0 ): 》For Turbine ( q = 0 ): 》For condenser ( w = 0 ): The thermal efficiency of Rankine Cycle is: How can we Increase the Efficiency of A Rankine Cycle: The efficiency of a Rankine cycle can be increased: Increasing the avg. temperate at which heat is added Decreasing the avg. Temperature at which heat is rejected. The above two objectives can be achieved by following three met...
Welded Joints A permanent joint which is obtained by the friction of edges of two parts to be joined, with or without the application of pressure and a filler material. Used in fabrication as an alternative method for casting and forging . Used as a repair medium . If filler material is used ↠ Strength of Joint > Base metal strength . If filler not used ↠ Joint strength < Base metal strength . Grinding Finish ↠ Welding at top and bottom off the plate. Machining Finish ↠ Welding at bottom surface after welding machining operation. Want to learn more about welded joint, click here . Designing of Butt Joint Design of Lap Joint or Fillet Joint Lap or Fillet joint is " formed by the overlapping of plates and then welding the edges of plates " . There are two types of fillet joints: Single and Double Transverse Fillet Joints ↣ are designed for tensile loading. Parallel Fillet Joints ↣ are designe...
Gear Forming by Machining Formation of gear through machining consists of following methods: Form Milling by Disc Cutter Form Milling by End Mill Cutter Shaper, Planner and Slotter Broaching 1. Form Milling by Disc Cutter It is defined as, " Tooth is cut one by one by plunging the rotating cutter into the blank " . Each gear needs a separate cutter. 8 - 10 standard cutters are available for producing 12 - 120 teeth gears. Used for big spur gears of large pitch. 2. Form Milling by End Mill Cutter It includes the cutting of tooth at a time and then indexed for the next tooth space for cutting. For a small volume production of low precision gears. Set of 10 cutters ↠ 12 - 120 teeth gears . Used for teeth of large gears/module. To reduce cost, same cutter is often used for multiple sized gears resulting in profile errors . Characteristics: Use of Hardened stainless steels (HSS) form milling cutters. Use of Ordinary milling machines. Low production rate (need of indexing...
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.