Theory of turbo machine Effect of Blade Configuration on Characteristics of Centrifugal machines. Unit 2 (Potters & Wiggert Sec
|
|
- Austen Lamb
- 5 years ago
- Views:
Transcription
1 Theory of turbo machine Effect of Blade Configuration on Characteristics of Centrifugal machines Unit (Potters & Wiggert Sec. 1..1, &-607)
2 Expression relating Q, H, P developed by Rotary machines Rotary Machines include: Centrifugal (or radial), Axial, and Mixed types In such machines when fluid passes through blade passage static pressure changes.
3 < Axial flow (Unit #4) Axial flow Mixed flow Centrifugal (Unit # )
4 CENTRIFUGAL MACHINE 1..1
5 A typical radial flow pump.
6 We already know from Mechanics 1. For a rotary machine Power = Angular velocity x Torque = Mass flow rate x Head Torque = Rate of change of angular momentum = Mass x [Abs. Circum. velocity x radius (in-out)] T = [ρ Q] (r V t r 1 V t1 )
7 (a) impeller; Idealized radial-flow impeller (b) velocity diagrams.
8 Relative Velocity (Fluid entering periphery)
9
10 Power (In terms of flow rate & Blade angle) From velocity triangle: V t = V n cotα = u V n cotβ where V n is radial component of V From above P = ρ Q(u V t u 1 V t1 ) = ρ Q(u V n cotα u 1 V n1 cotα 1 ) (5) NOTE 1. To minimize entrance loss Blade angle β is equal to the entry angle of fluid to the blade.. To minimize exit loss Fluid entry angle (α) is equal to the angle of the guide vane 3. α = Angle between tip and absolute velocity β = Angle between tip and relative velocity
11 Symbols to be used Velocities: V - Absolute fluid velocity v - Relative fluid velocity u - peripheral speed of blade Geometry: b - blade width r - blade radius α - angle between V and u vectors β - angle between v and u vectors t n Subscripts: 1 -inlet -outlet - normal component - tangential component
12 Head Power, P = Weight flow rate x Head = P = (ρ Qg) H Head of fluid column, H = P/(ρ Q.g)] (6) Substituting P from Eq.5 we get ( u V u V ) u V cotα u V cot (7) H = t 1 t1 ( n 1 n1 α1) For highest head cot α 1 = 0; i.e α 1 = 90 g uvt u( u Vn cot β) (8) H = = g g Substituting: Flow rate, Q = V n.π r b; Tip velocity u = wr, we can get ω r g (9) = ( ) H = ω cot β πb g Q g
13 Summary of what we have learnt From geometry V n = V -V t = v - (u V t ) u V t = (V + u v )/ (1) where u = velocity of blade, V t = tangential component of absolute velocity of fluid From (4) & (1) (13) Head = Kinetic energy gain + Pressure rise g V V u u g V V H g V u V V u V Qg P H r r r r ) ( ) ( ) ( = + + = = ρ
14 SUMMARY Blade angle (β) is ideally the angle between the relative velocity (V r ) and blade-tip velocity (u) vectors To draw the vector diagram note that the blade-tip velocity and relative velocity vector are in the same rotational (clockwise or anticlockwise) direction. Third side of the triangle is the absolute velocity vector which is in opposite direction. Power = [blade velocity x tangential component of absolute velocity] inlet outlet Flow ~ Rotor circumference x width x Normal velocity
15 What we have learnt Blade angle (β) is ideally the angle between the relative velocity (V r ) and blade-tip velocity (u) vectors To draw the vector diagram note that the blade-tip velocity and relative velocity vector are in the same rotational (clockwise or anticlockwise) direction. The arm of the triangle is the absolute velocity vector which is in opposite direction. Power = [blade velocity x tangential component of absolute velocity] inlet outlet Flow ~ Rotor circumference x width x Normal velocity
16 Blade shapes Straight (radial) blade wheel Forward curve wheel Backward curve wheel
17 Vector diagram of a centrifugal pump/fan
18 FLOW CHARACTERISTICS Head = Power delivered to fluid Fluid flow rate (weight) H = P w /(ρq g) = (u V t u 1 V t1 )/g For maximum head, V t1 = 0 Η = u V t /g From velocity diagram, V t = u -V n cotβ Flow rate discharge, Q = πr bv n So,H = [u -(Q/ πr b) u cotβ ]/g = A B.Q cotβ
19 Efficiency Ideal Head varies linearly with discharge (Q). Head (H) increases or decreases with Q depending on blade angle β With valve shut off. i.e Q = 0 For pumps/fans: Efficiency = where P is the power consumed η = H = u g ρqgh P
20 Ideal H vs Q characteristics
21 Effect of blade configuration on Performance Depending upon the value of exit blade angle the head increases or decreases with increase in flow Energy transfer ~ V t. From velocity diagram, for a given tip velocity, u forward & radial curve blades transfer more energy Backward blades give higher efficiency Forward and radial are smaller in size for the same duty, but have lower efficiency Centrifugal compressor uses radial blades for better strength against high speed rotation
22 Characteristics of different types Owing to the losses the actual characteristic is different from theoretical linear shape Power consumption varies with flow Q Efficiency varies with Q with highest value being in the design condition of blades
23 Home work 1. Show that the manometric head for a pump having a discharge Q and running at a speed N can be expressed by an equation of the form H m =AN +BNQ+CQ, where A,B,C are constants.
24 Example 1. A centrifugal pump impeller is 55 mm diameter, the water passage 3 mm wide at exit, and the vane angle at exit 30. The effective flow area is reduced by 10% because of vane thickness. The manometric efficiency is 80% when the pump runs at 1000 rpm and delivers 50 litre/s. Calculate the manometer head measured between inlet and outlet flange of the pump assuming 47% of the discharge head is not converted into pressure head. Assume the pump delivers maximum head.
Department of Civil and Environmental Engineering CVNG 1001: Mechanics of Fluids
INTRODUCTION Hydrodynamic Machines A hydromachine is a device used either for extracting energy from a fluid or to add energy to a fluid. There are many types of hydromachines and Figure 1 below illustrates
More informationENERGY TRANSFER BETWEEN FLUID AND ROTOR. Dr. Ir. Harinaldi, M.Eng Mechanical Engineering Department Faculty of Engineering University of Indonesia
ENERGY TRANSFER BETWEEN FLUID AND ROTOR Dr. Ir. Harinaldi, M.Eng Mechanical Engineering Department Faculty of Engineering University of Indonesia Basic Laws and Equations Continuity Equation m m ρ mass
More informationIntroduction to Fluid Machines (Lectures 49 to 53)
Introduction to Fluid Machines (Lectures 49 to 5) Q. Choose the crect answer (i) (ii) (iii) (iv) A hydraulic turbine rotates at N rpm operating under a net head H and having a discharge Q while developing
More informationIn this lecture... Centrifugal compressors Thermodynamics of centrifugal compressors Components of a centrifugal compressor
Lect- 3 In this lecture... Centrifugal compressors Thermodynamics of centrifugal compressors Components of a centrifugal compressor Centrifugal compressors Centrifugal compressors were used in the first
More information(Refer Slide Time: 4:41)
Fluid Machines. Professor Sankar Kumar Som. Department Of Mechanical Engineering. Indian Institute Of Technology Kharagpur. Lecture-30. Basic Principle and Energy Transfer in Centrifugal Compressor Part
More informationIntroduction to Turbomachinery
1. Coordinate System Introduction to Turbomachinery Since there are stationary and rotating blades in turbomachines, they tend to form a cylindrical form, represented in three directions; 1. Axial 2. Radial
More informationLect 22. Radial Flow Turbines. Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay
Lecture Lect Radial Flow Turbines Lect Radial inflow turbines, which look similar to centrifugal compressor, are considered suitable for application in small aircraft engines. In many applications a radial
More informationChapter Four Hydraulic Machines
Contents 1- Introduction. - Pumps. Chapter Four Hydraulic Machines (لفرع الميكانيك العام فقط ( Turbines. -3 4- Cavitation in hydraulic machines. 5- Examples. 6- Problems; sheet No. 4 (Pumps) 7- Problems;
More informationMECA-H-402: Turbomachinery course Axial compressors
MECA-H-40: Turbomachinery course Axial compressors Pr. Patrick Hendrick Aero-Thermo-Mecanics Year 013-014 Contents List of figures iii 1 Axial compressors 1 1.1 Introduction...............................
More information(Refer Slide Time: 0:45)
(Refer Slide Time: 0:45) Fluid Machines. Professor Sankar Kumar Som. Department Of Mechanical Engineering. Indian Institute Of Technology Kharagpur. Lecture-3. Impulse and Reaction Machines: Introductory
More informationChapter Four Hydraulic Machines
Contents 1- Introduction. 2- Pumps. Chapter Four Hydraulic Machines (لفرع الميكانيك العام فقط ( Turbines. -3 4- Cavitation in hydraulic machines. 5- Examples. 6- Problems; sheet No. 4 (Pumps) 7- Problems;
More informationIntroduction to Fluid Machines and Compressible Flow Prof. S.K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur
Introduction to Fluid Machines and Compressible Flow Prof. S.K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture No. # 24 Axial Flow Compressor Part I Good morning
More informationCHAPTER TWO CENTRIFUGAL PUMPS 2.1 Energy Transfer In Turbo Machines
7 CHAPTER TWO CENTRIFUGAL PUMPS 21 Energy Transfer In Turbo Machines Fig21 Now consider a turbomachine (pump or turbine) the total head (H) supplied by it is The power delivered to/by the fluid simply
More informationM E 320 Professor John M. Cimbala Lecture 23
M E 320 Professor John M. Cimbala Lecture 23 Today, we will: Discuss diffusers and do an example problem Begin discussing pumps, and how they are analyzed in pipe flow systems D. Diffusers 1. Introduction.
More informationBASIC EQUATION. Rotational speed. u = linear velocity in m/s r = radius in m ω = angular velocity in rad/s D = diameter in m N = rotation per minute
CENTRIFUGAL PUMP BASIC EQUATION Rotational speed u = rω = πdn 60 u = linear velocity in m/s r = radius in m ω = angular velocity in rad/s D = diameter in m N = rotation per minute Power Power = F V = P
More informationIntroduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur
Introduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 21 Centrifugal Compressor Part I Good morning
More informationConservation of Angular Momentum
10 March 2017 Conservation of ngular Momentum Lecture 23 In the last class, we discussed about the conservation of angular momentum principle. Using RTT, the angular momentum principle was given as DHo
More informationmywbut.com Hydraulic Turbines
Hydraulic Turbines Hydro-electric power accounts for up to 0% of the world s electrical generation. Hydraulic turbines come in a variety of shapes determined by the available head and a number of sizes
More informationRadial Compressors. Damian Vogt Course MJ2429. Nomenclature
Turbomachinery Lecture Notes 1 007-10-04 Radial Compressors Damian Vogt Course MJ49 Nomenclature Subscripts Symbol Denotation Unit c Absolute velocity m/s h Enthalpy J/kg m& Mass flow rate kg/s r Radius
More informationLect-33. In this lecture... Tutorial on centrifugal compressors. Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay
Let- 33 In this leture... Let-33 utorial on entrifugal ompressors Problem # At the inlet of a entrifugal ompressor eye, the relative Mah number is to be limited to 0.97. he hub-tip radius ratio of the
More informationProf. Dr.-Ing. F.-K. Benra. ISE batchelor course
University Duisburg-Essen Campus Duisburg Faculty of engineering Science Department of Mechanical Engineering Examination: Fluid Machines Examiner: Prof. Dr.-Ing. F.-K. Benra Date of examination: 06.03.2006
More informationnozzle which is fitted to a pipe through which the liquid is flowing under pressure.
Impact of Jets 1. The liquid comes out in the form of a jet from the outlet of a nozzle which is fitted to a pipe through which the liquid is flowing under pressure. The following cases of the impact of
More informationIn this lecture... Radial flow turbines Types of radial flow turbines Thermodynamics and aerodynamics Losses in radial flow turbines
Lect- 35 1 In this lecture... Radial flow turbines Types of radial flow turbines Thermodynamics and aerodynamics Losses in radial flow turbines Radial turbines Lect-35 Development of radial flow turbines
More informationSOE2156: Fluids Lecture 4
Turbo SOE2156: s Lecture 4 machine { a device exchanging energy (work) between a uid and a mechanical system. In particular : a turbomachine is a device using a rotating mechanical system. The ow of energy
More informationBASIC EQUATION. Rotational speed = = ABC 60
CENTRIFUGAL PUMP BASIC EQUATION Rotational speed = =?@ = ABC 60 = = linear velocity in m/s? = radius in m @ = angular velocity in rad/s B = diameter in m C = rotation per minute Power OPQR? = S U = O V
More informationSpecific Static rotor work ( P P )
The specific Static Rotor ork p 1 ρ Specific Static rotor work ( P P ) here P, P static pressures at points, (P P ) static pressure difference of the rotor ρ density, in case of a compressible medium average
More informationCentrifugal Machines Table of Contents
NLNG Course 017 Table of Contents 1 Introduction and Basic Principles... 1.1 Hydraulic Machines... 1.... 1.3 Pump Geometry... 1.4 Pump Blade Geometry...3 1.5 Diffusers...5 1.6 Pump Losses...6 1.7 Example
More informationIntroduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur
Introduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 1 Introduction to Fluid Machines Well, good
More informationCHAPTER EIGHT P U M P I N G O F L I Q U I D S
CHAPTER EIGHT P U M P I N G O F L I Q U I D S Pupmps are devices for supplying energy or head to a flowing liquid in order to overcome head losses due to friction and also if necessary, to raise liquid
More informationTheory of turbo machinery / Turbomaskinernas teori. Dixon, chapter 7. Centrifugal Pumps, Fans and Compressors
Theory of turbo machinery / Turbomaskinernas teori Dixon, chapter 7 Centrifugal Pumps, Fans and Compressors And to thy speed add wings. (MILTON, Paradise Lost.) What do radial machines look like? Swept
More informationDr. S. Ramachandran Prof. R. Devaraj. Mr. YVS. Karthick AIR WALK PUBLICATIONS
Fluid Machinery As per Revised Syllabus of Leading Universities including APJ ABDUL KALAM TECHNOLOGICAL UNIVERSITY Dr. S. Ramachandran Prof. R. Devaraj Professors School of Mechanical Engineering Sathyabama
More informationME 316: Thermofluids Laboratory
ME 316 Thermofluid Laboratory 6.1 KING FAHD UNIVERSITY OF PETROLEUM & MINERALS ME 316: Thermofluids Laboratory PELTON IMPULSE TURBINE 1) OBJECTIVES a) To introduce the operational principle of an impulse
More informationIntroduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur
Introduction to Fluid Machines and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 07 Analysis of Force on the Bucket of Pelton
More information9. Pumps (compressors & turbines) Partly based on Chapter 10 of the De Nevers textbook.
Lecture Notes CHE 31 Fluid Mechanics (Fall 010) 9. Pumps (compressors & turbines) Partly based on Chapter 10 of the De Nevers textbook. Basics (pressure head, efficiency, working point, stability) Pumps
More informationASSESSMENT OF DESIGN METHODOLOGY AND THREE DIMENSIONAL NUMERICAL (CFD) ANALYSIS OF CENTRIFUGAL BLOWER
ASSESSMENT OF DESIGN METHODOLOGY AND THREE DIMENSIONAL NUMERICAL (CFD) ANALYSIS OF CENTRIFUGAL BLOWER D. R. Chaudhari 1, H. N. Patel 2 1,2 Mechanical Department, Government Engineering College Dahod, (India)
More informationIntroduction to Fluid Machines, and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur
Introduction to Fluid Machines, and Compressible Flow Prof. S. K. Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 09 Introduction to Reaction Type of Hydraulic
More informationCE 6403 APPLIED HYDRAULIC ENGINEERING UNIT - V PUMPS
CE 6403 APPLIED HYDRAULIC ENGINEERING UNIT - V PUMPS Centrifugal pups - Miniu speed to start the pup - NPSH - Cavitations in pups Operating characteristics - Multistage pups - Reciprocating pups - Negative
More informationNumerical Study of the Semi-Open Centrifugal Pump Impeller Side Clearance A. Farid Ayad *, H. M. Abdalla,A. S. Abo El-Azm Egyptian Armed Forces, Egypt
16 th International Conference on AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 May 26-28, 2015, E-Mail: asat@mtc.edu.eg Military Technical College, Kobry Elkobbah, Cairo, Egypt Tel : +(202) 24025292
More informationVentilation 5 Fans Vladimír Zmrhal (room no. 814) http://users.fs.cvut.cz/~zmrhavla/index.htm Dpt. Of Environmental Engineering 1 Introduction Fans air pump that creates a pressure difference and causes
More informationLaboratory Notes. Turbomachinery
Brussels School of Engineering École polytechnique de Bruxelles Academic Year 2016-2017 Laboratory Notes Turbomachinery Aero-Thermo-Mechanics Department Teaching Assistants : Laurent Ippoliti Joëlle Vincké
More informationContents. 2 Basic Components Aerofoils Force Generation Performance Parameters xvii
Contents 1 Working Principles... 1 1.1 Definition of a Turbomachine... 1 1.2 Examples of Axial Turbomachines... 2 1.2.1 Axial Hydraulic Turbine... 2 1.2.2 Axial Pump... 4 1.3 Mean Line Analysis... 5 1.4
More informationProf. Dr.-Ing. F.-K. Benra. ISE Bachelor Course
University Duisburg-Essen Campus Duisburg Faculty of Engineering Science Examination: Fluid Machines Examiner: Prof. Dr.-Ing. F.-K. Benra Date of examination: 07.08.2006 Handling time: 120 Minutes ISE
More informationEFFECT OF FORCED ROTATING VANELESS DIFFUSERS ON CENTRIFUGAL COMPRESSOR STAGE PERFORMANCE
Journal of Engineering Science and Technology Vol. 6, No. 5 (2011) 558-574 School of Engineering, Taylor s University EFFECT OF FORCED ROTATING VANELESS DIFFUSERS ON CENTRIFUGAL COMPRESSOR STAGE PERFORMANCE
More informationTheoretical, Experimental and Numerical Investigations of the Effect of Blades Number on the Performance of Regenerative Blowers
Theoretical, Experimental and Numerical Investigations of the Effect of Blades Number on the Performance of Regenerative Blowers T. 1 Mekhail, O. 2 Dahab, M. 1 Fathy, M. 3 EL-Gendi, and H. 1* Abdel-Mohsen
More information3 Energy Exchange in Turbomachines
3 Energy Exchange in Turbomachines Problem 1 The solved and unsolved examples of this chapter are meant to illustrate the various forms of velocity triangles and the variety of the turbomachines. In addition,
More informationLect-36. In this lecture... Tutorial on radial flow turbines. Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay
Lect- 36 1 In this lecture... Lect-36 Tutorial on radial flow turbines 2 Problem # 1 Lect-36 The rotor of an IFR turbine, which is designed to operate at the nominal condition, is 23.76 cm in diameter
More informationChapter (6) Energy Equation and Its Applications
Chapter (6) Energy Equation and Its Applications Bernoulli Equation Bernoulli equation is one of the most useful equations in fluid mechanics and hydraulics. And it s a statement of the principle of conservation
More informationCOMPUTER AIDED DESIGN OF RADIAL TIPPED CENTRIFUGAL BLOWERS AND FANS
4 th International Conference on Mechanical Engineering, December 26-28, 21, Dhaka, Bangladesh/pp. IV 55-6 COMPUTER AIDED DESIGN OF RADIAL TIPPED CENTRIFUGAL BLOWERS AND FANS Nitin N. Vibhakar* and S.
More informationTHEORETICAL MODEL FOR PREDICTING AXIAL FANS/BLOWERS PERFORMANCE CHARACTERISTICS
International Journal of Mechanical And Production Engineering, ISSN: 30-09, Volume- 3, Issue-, Feb.-015 THEORETICAL MODEL FOR PREDICTING AXIAL FANS/BLOWERS PERFORMANCE CHARACTERISTICS OMBOR PEREOWEI GARRICK
More informationProf. Dr.-Ing. F.-K. Benra. ISE Bachelor Course
University Duisburg-Essen Campus Duisburg Faculty of Engineering Science Department of Mechanical Engineering Name Matr.- Nr. Examination: Fluid Machines Examiner: Prof. Dr.-Ing. F.-K. Benra Date of examination:
More informationFlow analysis in centrifugal compressor vaneless diffusers
348 Journal of Scientific & Industrial Research J SCI IND RES VOL 67 MAY 2008 Vol. 67, May 2008, pp. 348-354 Flow analysis in centrifugal compressor vaneless diffusers Ozturk Tatar, Adnan Ozturk and Ali
More informationChapter Two. Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency. Laith Batarseh
Chapter Two Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency Laith Batarseh The equation of continuity Most analyses in this book are limited to one-dimensional steady flows where the velocity
More informationStudy on the Performance of a Sirocco Fan (Flow Around the Runner Blade)
Rotating Machinery, 10(5): 415 424, 2004 Copyright c Taylor & Francis Inc. ISSN: 1023-621X print / 1542-3034 online DOI: 10.1080/10236210490474629 Study on the Performance of a Sirocco Fan (Flow Around
More informationPlease welcome for any correction or misprint in the entire manuscript and your valuable suggestions kindly mail us
Problems of Practices Of Fluid Mechanics Compressible Fluid Flow Prepared By Brij Bhooshan Asst. Professor B. S. A. College of Engg. And Technology Mathura, Uttar Pradesh, (India) Supported By: Purvi Bhooshan
More informationApplied Fluid Mechanics
Applied Fluid Mechanics 1. The Nature of Fluid and the Study of Fluid Mechanics 2. Viscosity of Fluid 3. Pressure Measurement 4. Forces Due to Static Fluid 5. Buoyancy and Stability 6. Flow of Fluid and
More informationLecture-10 Tutorial -2 Solved Problems and Tutorial Problems On Three Dimensional flow in Axial Flow Compressor
1 Lecture-10 Tutorial -2 Solved Problems and Tutorial Problems On Three Dimensional flow in Axial Flow Compressor 2 Recap of simple 3-D flow theories (These are mainly used for design) Lect-10 1)Free Vortex
More informationIJREAS Volume 2, Issue 2 (February 2012) ISSN:
DESIGN AND CFD ANALYSIS OF SINGLE STAGE, END SUCTION, RADIAL FLOW CENTRIFUGAL PUMP FOR MINE DEWATERING APPLICATION Swapnil Urankar * Dr. H S Shivashankar ** Sourabh Gupta *** ABSTRACT Heavy centrifugal
More informationConsider a control volume in the form of a straight section of a streamtube ABCD.
6 MOMENTUM EQUATION 6.1 Momentum and Fluid Flow In mechanics, the momentum of a particle or object is defined as the product of its mass m and its velocity v: Momentum = mv The particles of a fluid stream
More informationChapter 8 COOLING AND HEAT TRANSFER. 8.1 Importance of thermal analysis. 8.2 Heat transfer modes
Chapter 8 COOLING AND HEAT TRANSFER 8.1 Importance of thermal analysis During the operation of an electrical machine, heat is generated due to power losses in electric and magnetic circuits and mechanical
More information4 Mechanics of Fluids (I)
1. The x and y components of velocity for a two-dimensional flow are u = 3.0 ft/s and v = 9.0x ft/s where x is in feet. Determine the equation for the streamlines and graph representative streamlines in
More informationFluid Structural Analysis of Centrifugal FAN Using FEA
Fluid Structural Analysis of Centrifugal FAN Using FEA Uppada Umamaheswara Rao M.Tech (Machine Design) Malla Reddy College of Engineering and Technology, JNTU, Hyderabad, Telangana, India. ABSTRACT In
More informationAn improved theory for regenerative pump performance
213 An improved theory for regenerative pump performance T Meakhail and S O Park Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Taejon, Republic of Korea The manuscript
More informationCENTRIFUGAL PUMP SELECTION, SIZING, AND INTERPRETATION OF PERFORMANCE CURVES
CENTRIFUGAL PUMP SELECTION, SIZING, AND INTERPRETATION OF PERFORMANCE CURVES 4.0 PUMP CLASSES Pumps may be classified in two general types, dynamic and positive displacement. Positive displacement pumps
More informationOptimizing Centrifugal Pump Performance by Different Blade Configuration Patterns
American Journal of Mechanical and Industrial Engineering 2018; 3(1): 1-14 http://www.sciencepublishinggroup.com/j/ajmie doi: 10.11648/j.ajmie.20180301.11 ISSN: 2575-6079 (Print); ISSN: 2575-6060 (Online)
More informationDesign of Multistage Turbine
Turbomachinery Lecture Notes 7-9-4 Design of Multistage Turbine Damian Vogt Course MJ49 Nomenclature Subscripts Symbol Denotation Unit c Absolute velocity m/s c p Specific heat J/kgK h Enthalpy J/kg m&
More informationStator Blade Motor Motor Housing
The internal workings of a Ducted Fan The rotor velocity vectors and blade angles After looking at EDFs from a pure axial change of momentum position we must now address the question how the fan is shaped
More informationPhys101 Lectures 19, 20 Rotational Motion
Phys101 Lectures 19, 20 Rotational Motion Key points: Angular and Linear Quantities Rotational Dynamics; Torque and Moment of Inertia Rotational Kinetic Energy Ref: 10-1,2,3,4,5,6,8,9. Page 1 Angular Quantities
More informationDynamic centrifugal compressor model for system simulation
Journal of Power Sources xxx (2005) xxx xxx Dynamic centrifugal compressor model for system simulation Wei Jiang, Jamil Khan, Roger A. Dougal Department of Mechanical Engineering, University of South Carolina,
More informationDesign of Radial Turbines & Turbochargers
RMD50 Design of Radial Turbines & Turbochargers Session delivered by: Prof. Q. H. Nagpurwala 4 @ M S Ramaiah School of Advanced Studies, Bengaluru Session Objective RMD50 To discuss the design of radial
More informationInternational Journal of Research in Advent Technology Available Online at:
A COMPUTER PROGRAMMED DESIGN OPTIMISATION AND ANALYSIS OF COMPRESSOR IMPELLER G. Naga Malleshwar Rao 1, Dr. S.L.V. Prasad 2, Dr. S. Sudhakarbabu 3 1, 2 Professor of Mechanical Engineering, Shri Shirdi
More information(Refer Slide Time: 0:57)
Fluid Dynamics And Turbo Machines. Professor Dr Dhiman Chatterjee. Department Of Mechanical Engineering. Indian Institute Of Technology Madras. Part B. Module-2. Lecture-4. Representation of Turbo Machines
More informationby Dr. Shibayan Sarkar Department of Mechanical Engineering
Lecture on Pump by Dr. Shibayan Sarkar Department of Mechanical Engineering Indian School of Mines Dhanbad WHAT IS PUMP? A hydrodynamic pump machine is a device which converts the mechanical energy held
More informationChapter 8 Lecture. Pearson Physics. Rotational Motion and Equilibrium. Prepared by Chris Chiaverina Pearson Education, Inc.
Chapter 8 Lecture Pearson Physics Rotational Motion and Equilibrium Prepared by Chris Chiaverina Chapter Contents Describing Angular Motion Rolling Motion and the Moment of Inertia Torque Static Equilibrium
More informationAxial Flow and Radial Flow Gas Turbines
7 Axial Flow and Radial Flow Gas Turbines 7.1 INTRODUCTION TO AXIAL FLOW TURBINES The axial flow gas turbine is used in almost all applications of gas turbine power plant. Development of the axial flow
More informationCFD approach for design optimization and validation for axial flow hydraulic turbine
Indian Journal of Engineering & Materials Sciences Vol. 16, August 009, pp. 9-36 CFD approach for design optimization and validation for axial flow hydraulic turbine Vishnu Prasad, V K Gahlot* & P Krishnamachar
More informationAxial Flow Compressors and Fans
5 Axial Flow Compressors and Fans 5.1 INTRODUCTION As mentioned in Chapter 4, the maximum pressure ratio achieved in centrifugal compressors is about 4:1 for simple machines (unless multi-staging is used)
More informationEXPERIMENT No.1 FLOW MEASUREMENT BY ORIFICEMETER
EXPERIMENT No.1 FLOW MEASUREMENT BY ORIFICEMETER 1.1 AIM: To determine the co-efficient of discharge of the orifice meter 1.2 EQUIPMENTS REQUIRED: Orifice meter test rig, Stopwatch 1.3 PREPARATION 1.3.1
More informationCentrifugal Pumps. Problem 1. This is a small project having three parts: Parts (a), (b), and (c).
7 Centrifugal Pumps Problem 1 This is a small project having three parts: Parts (a), (b), and (c). Part (a): Enlist the design parameters and performance parameters of a centrifugal pump. Explain, to the
More informationChapter three. Two-dimensional Cascades. Laith Batarseh
Chapter three Two-dimensional Cascades Laith Batarseh Turbo cascades The linear cascade of blades comprises a number of identical blades, equally spaced and parallel to one another cascade tunnel low-speed,
More informationINSTITUTE OF AERONAUTICAL ENGINEERING
LECTURE NOTES ON Hydraulics and Hydraulic Machines Department of Civil Engineering INSTITUTE OF AERONAUTICAL ENGINEERING Dundigal 500 043, Hyderabad mechanis m COURTESY IARE Governors for Turbines Pendulum
More informationResearch on energy conversion mechanism of a screw centrifugal pump under the water
IOP Conference Series: Materials Science and Engineering OPEN ACCESS Research on energy conversion mechanism of a screw centrifugal pump under the water To cite this article: H Quan et al 213 IOP Conf.
More informationChapter 4. Turbomachinery. 4.1 Introduction. 4.2 Pumps
Chapter 4 Turbomachinery 4.1 Introduction In this chapter we will examine the performance characteristics of turbomachinery. The word turbo implies a spinning action is involved. In turbomachinery, a blade
More informationChapter 7 Steam Turbines MEE 325 Power Plants Engineering
Chapter 7 Steam Turbines MEE 325 Power Plants Engineering Atikorn W. Mechanical Engineering Department King Mongkut s University of Technology Thonburi Introduction Steam turbine is an energy conversion
More informationvector H. If O is the point about which moments are desired, the angular moment about O is given:
The angular momentum A control volume analysis can be applied to the angular momentum, by letting B equal to angularmomentum vector H. If O is the point about which moments are desired, the angular moment
More informationCOMPUTATIONAL FLOW ANALYSIS THROUGH A DOUBLE-SUCTION IMPELLER OF A CENTRIFUGAL PUMP
Proceedings of the Fortieth National Conference on Fluid Mechanics and Fluid Power December 12-14, 2013, NIT Hamirpur, Himachal Pradesh, India FMFP2013_141 COMPUTATIONAL FLOW ANALYSIS THROUGH A DOUBLE-SUCTION
More informationCHAPTER 12 Turbomachinery
CAER urbomachinery Chapter / urbomachinery 800 / 0 8 8 rad /s, u r 8 8 0 0 m /s, u r 8 8 0 0 8 m /s, rbv, but V u since, n n 0 0 0 0 0 0 m / s V V 0 0 m /s, rb 0 0 0 Vn u 0 8 6 77 m /s, tan tan 0 n t V
More informationHYDRAULIC TURBINES. Hydraulics and Hydraulic Machines
HYDRAULIC TURBINES Introduction: The device which converts h ydraulic energy into mechanical energy or vice versa is known as Hydraulic Machines. The h ydraulic machines which convert h ydraulic energy
More informationDesign of Monoblock Centrifugal Pump Impeller
Design of Monoblock Centrifugal Pump Impeller Authors Mr. Chetan Kallappa Tambake 1, Prof. P. V. Salunke 1 Department of Mechanical Engineering, Walchand Institute of Technology, Ashok Chowk, Solapur-413006,
More informationBernoulli s equation may be developed as a special form of the momentum or energy equation.
BERNOULLI S EQUATION Bernoulli equation may be developed a a pecial form of the momentum or energy equation. Here, we will develop it a pecial cae of momentum equation. Conider a teady incompreible flow
More informationPerformance characteristics of turbo blower in a refuse collecting system according to operation conditions
Journal of Mechanical Science and Technology 22 (2008) 1896~1901 Journal of Mechanical Science and Technology www.springerlink.com/content/1738-494x DOI 10.1007/s12206-008-0729-6 Performance characteristics
More informationImpact of a Jet. Experiment 4. Purpose. Apparatus. Theory. Symmetric Jet
Experiment 4 Impact of a Jet Purpose The purpose of this experiment is to demonstrate and verify the integral momentum equation. The force generated by a jet of water deflected by an impact surface is
More informationCFD Analysis of Centrifugal Pump in Sewerage System
CFD Analysis of Centrifugal Pump in Sewerage System J. Beston 1, G. Gopi 1, S. Gopi 1, M. Karthika 1, Dr. S. V. Suresh Babu 2 1 Department of Mechanical Engineering, Adhiyamaan College of Engineering,
More informationUNIFIED DESIGN AND COMPARATIVE PERFORMANCE EVALUATION OF FORWARD AND BACKWARD CURVED RADIAL TIPPED CENTRIFUGAL FAN
Proceedings of the International Conference on Mechanical Engineering 3 (ICME3) 6-8 December 3, Dhaka, Bangladesh ICME3-FL- UNIFIED DESIGN AND COMPARATIVE PERFORMANCE EVALUATION OF FORWARD AND BACKWARD
More informationCOURSE CODE : 3072 COURSE CATEGORY : B PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE
COURSE TITLE : FLUID MECHANICS COURSE CODE : 307 COURSE CATEGORY : B PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE MODULE TOPIC PERIOD 1 Properties of Fluids 0 Fluid Friction and Flow
More informationTheory and Applica0on of Gas Turbine Systems
Theory and Applica0on of Gas Turbine Systems Part IV: Axial and Radial Flow Turbines Munich Summer School at University of Applied Sciences Prof. Kim A. Shollenberger Introduc0on to Turbines Two basic
More informationME332 FLUID MECHANICS LABORATORY (PART II)
ME332 FLUID MECHANICS LABORATORY (PART II) Mihir Sen Department of Aerospace and Mechanical Engineering University of Notre Dame Notre Dame, IN 46556 Version: April 2, 2002 Contents Unit 5: Momentum transfer
More informationAkshay Khadse, Lauren Blanchette, Mahmood Mohagheghi, Jayanta Kapat
Impact of S-CO2 Properties on Centrifugal Compressor Impeller: Comparison of Two Loss Models for Mean Line Analyses The Supercritical CO2 Power Cycles Symposium 2016 Akshay Khadse, Lauren Blanchette, Mahmood
More informationDESIGN AND CFD ANALYSIS OF A CENTRIFUGAL PUMP
DESIGN AND CFD ANALYSIS OF A CENTRIFUGAL PUMP 1 CH.YADAGIRI, 2 P.VIJAYANAND 1 Pg Scholar, Department of MECH, Holymary Institute of Technology, Ranga Reddy, Telangana, India. 2 Assistant Professor, Department
More informationLecture on Francis Turbine. by Dr. Shibayan Sarkar Department of Mechanical Engg Indian Institute of Technology (ISM), Dhanbad
Lecture on Francis Turbine by Dr. Shibayan Sarkar Department of Mechanical Engg Indian Institute of Technology (ISM), Dhanbad Turbines: Francis (1849) di, Qo Ri ɵ Ra Stay ring Spiral casing π Q = v d 4
More informationPerformance Investigation of High Pressure Ratio Centrifugal Compressor using CFD
International Journal of Ignited Minds (IJIMIINDS) Performance Investigation of High Pressure Ratio Centrifugal Compressor using CFD Manjunath DC a, Rajesh b, Dr.V.M.Kulkarni c a PG student, Department
More information