SlideShare a Scribd company logo
1 of 23
Vortex Shedding from a Group of
Cylinders
ENG 3163: BEng Final Year
Project
Individual work carried by: Youssef Sayed
Project Supervisor: Dr. Matteo Carpentieri
Problem Statement
 Flow around a circular cylinder has been a classic problem
in the fluid mechanics field where lots of experiments have
been carried on to understand the flow around it.
Research Objectives
 This project aims to investigate experimentally and discuss
theoretically the behaviour of the wake resulting from
different cylinder formations:
- Side by side
- Tandem
- Staggered
 Optimise the visualisation technique and the recording
systems used during the experiments.
 Forming a library of video-clips to be added to the existing
set of the EnFlo laboratory album.
Wake Configuration
Wake Configuration has been debated between many
engineers:
-Williamson (1985) discussed the two types of wake configuration
-Landweber (1942) found that all the vortex shedding are mainly inphase
-Thomas & Kraus (1964) detected the formation of inphase and antiphase
shedding
-Bearman & Wadcock (1973) and Quadflieg (1977) found preponderance
of the antiphase type of shedding.
Side by side Configuration
Two main approximations are the diameter of the cylinders
which is noted by ‘D’ and the gap width between the cylinders
noted by ‘T’
Side by side Configuration
Three observations have been noted by Sumner (2010)
regarding these formed patterns.
(a) The single bluff body ( T/D< 0.2)
(b) The based flow pattern (0.2< T/D < 2)
(c) Parallel vortex pattern ( T/D> 2)
Tandem Configuration
Two main approximations are the diameter of the cylinders,
noted by ‘D’, and the distance between the centre of the
cylinders, known as the centre width noted by ‘L’
Staggered Configuration
Three observations have been noted by Sumner (2010)
regarding these formed patterns.
Regime Zdravkovich (1987) Zhou & Yiu (2006)
Extended Body
Regime
1< L/D <1.2-1.8 1< L/D <2
Extended Body
Regime
1.2-1.8< L/D <3.4-3.8 2< L/D <5
Extended Body
Regime
L/D >3.4-3.8 L/D >5
Staggered Configuration
The staggered configuration is arrangement of two circular
cylinders; the geometry of this configuration is set by the
P/D dimensionless ratio and the angle of incidence α
Staggered Configuration
Four Groups identified by Sumner (2010)
Experimental Methodology Modification
1. New towing tank filling mechanism
Optimising the Recording Mechanism:
1. New flow control device
Experimental Methodology Modification
Optimising the Recording Mechanism:
2. Introducing the white sheet
Experimental Methodology Modification
Support Arms (Tandem configuration)
Experimental Methodology Modification
Results
The results were divided between two phases:
First phase experiments:
– Response from one cylinder
• (a) Testing best angle of injection
• (b) Effect of Reynolds number
• (c) Development of Vortex Street
– Response of cylinders arranged in side by side configuration
• (a) Effect of Proximity
• (b) Increase Reynolds number
• (c) Effect of Increasing Reynolds number with proximity
Second phase includes:
– Response of cylinders arranged in tandem configuration
• (a) Effect of Proximity
• (b) Effect of Increasing Reynolds number with proximity
Phase One Results
Results from the response of one cylinder
Selected flow options:
Injection =180 deg (Immediate Shedding)
Reynolds number =185 (Clear Flow)
Phase One Results
Results from the response of two cylinder (proximity effect)
Cylinders =2
Re =185
proximity=4D
Cylinders =2
Re =185
proximity=2D
Cylinders =2
Re =185
proximity=1D
Cylinders =2
Re =185
proximity=0.5D
Phase One Results
Results from the response of two cylinder (Re number effect)
Cylinders =2
Re =320
proximity=1D
Cylinders =2
Re =450
proximity=1D
Cylinders =2
Re =450
proximity=2D
Cylinders =2
Re =320
proximity=2D
Phase One Results
Results from the response of multiple cylinders (Increase
number of cylinders effect)
Cylinders =3
Re =185
proximity=1D
Cylinders =4
Re =185
proximity=1D
Cylinders =5
Re =185
proximity=1D
Phase Two Results
Results from the response of two cylinders (proximity effect)
Dis=1L/D Dis=2L/D Dis=3L/D Dis=3.5L/D Dis=4.5L/D Dis=5.5L/D
Phase Two Results
Results from the response of two cylinders (proximity effect)
Dis=1L/D Dis=3.5L/D Dis=4.5L/D Dis=5.5L/D
• Re= 320
• Re= 450
Conclusion and Observations
The results were divided between two phases:
Phase one observations:
 Predominance of the antiphase shedding wake configuration proving the
theory of Bearman & Wadcock (1973) and Quadflieg (1977).
 Proximities tested using two cylinders (side by side configuration) verified the
three flow pattern
 Intermediate cylinder using odd number of cylinders, showed anti-phase
shedding to both sides of the cylinder.
 When an even number of bodies were tested, the two cylinders spaced close
together showed an anti-phase shedding nature
Phase two observations :
 The proximities tested verified three regimes and demonstrated values that
are closer to Zhou & Yiu (2006)
 The co-shedding system recognised by Igrashi (1981) can have either
symmetrical or unsymmetrical mixing.
Thank you for your attention

More Related Content

Viewers also liked

Vibration control system
Vibration control systemVibration control system
Vibration control systemKok Kei Liew
 
Justifying a GEP Stack Height Taller than the EPA Formula Height
Justifying a GEP Stack Height Taller than the EPA Formula HeightJustifying a GEP Stack Height Taller than the EPA Formula Height
Justifying a GEP Stack Height Taller than the EPA Formula HeightRon Petersen, PhD, CCM, FASHRAE
 
Effect of wind Load On High Rise Building
Effect of wind Load On High Rise BuildingEffect of wind Load On High Rise Building
Effect of wind Load On High Rise BuildingVikas Patre
 
Scaffold classes and duties (cals)
Scaffold classes and duties (cals)Scaffold classes and duties (cals)
Scaffold classes and duties (cals)robadet
 

Viewers also liked (8)

Vibration control system
Vibration control systemVibration control system
Vibration control system
 
Tuned mass damper
Tuned mass damperTuned mass damper
Tuned mass damper
 
Wind Actions According To EC1
Wind Actions According To  EC1Wind Actions According To  EC1
Wind Actions According To EC1
 
TLD
TLDTLD
TLD
 
Justifying a GEP Stack Height Taller than the EPA Formula Height
Justifying a GEP Stack Height Taller than the EPA Formula HeightJustifying a GEP Stack Height Taller than the EPA Formula Height
Justifying a GEP Stack Height Taller than the EPA Formula Height
 
ETABS manual - Seismic design of steel buildings according to Eurocode 3 & 8
ETABS manual - Seismic design of steel buildings according to Eurocode 3 & 8 ETABS manual - Seismic design of steel buildings according to Eurocode 3 & 8
ETABS manual - Seismic design of steel buildings according to Eurocode 3 & 8
 
Effect of wind Load On High Rise Building
Effect of wind Load On High Rise BuildingEffect of wind Load On High Rise Building
Effect of wind Load On High Rise Building
 
Scaffold classes and duties (cals)
Scaffold classes and duties (cals)Scaffold classes and duties (cals)
Scaffold classes and duties (cals)
 

Similar to YOUSSEF_IND

CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDERCFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDERAM Publications
 
Stress Analysis on Split Ring
Stress Analysis on Split RingStress Analysis on Split Ring
Stress Analysis on Split RingIRJET Journal
 
Final Presentation_Ekramul_Haque_Ehite_04042016
Final Presentation_Ekramul_Haque_Ehite_04042016Final Presentation_Ekramul_Haque_Ehite_04042016
Final Presentation_Ekramul_Haque_Ehite_04042016Ekramul Haque Ehite
 
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...iosrjce
 
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...Khusro Kamaluddin
 
projetcs&contributions
projetcs&contributionsprojetcs&contributions
projetcs&contributionsLiu Huang
 
Energy Conversion Analysis Webinar
Energy Conversion Analysis WebinarEnergy Conversion Analysis Webinar
Energy Conversion Analysis WebinarEngineering Software
 
Development and design validation of pneumatic tool for stem seal collet fi...
Development and design validation of pneumatic tool for stem seal   collet fi...Development and design validation of pneumatic tool for stem seal   collet fi...
Development and design validation of pneumatic tool for stem seal collet fi...Dr.Vikas Deulgaonkar
 
Design, CFD Analysis and Fabrication of Solar Flat Plate Collector
Design, CFD Analysis and Fabrication of Solar Flat Plate CollectorDesign, CFD Analysis and Fabrication of Solar Flat Plate Collector
Design, CFD Analysis and Fabrication of Solar Flat Plate CollectorIRJET Journal
 
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDER
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDERCFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDER
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDERIRJET Journal
 
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...Ijripublishers Ijri
 
PhD_Annual_Review_2023.pdf
PhD_Annual_Review_2023.pdfPhD_Annual_Review_2023.pdf
PhD_Annual_Review_2023.pdfclaudiogcaccia
 
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...ijmech
 
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension System
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension SystemDesign and Performance Analysis of Mechanical Hydro Pneumatic Suspension System
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension SystemIRJET Journal
 
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...SEHER OZKAN
 

Similar to YOUSSEF_IND (20)

CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDERCFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
CFD and EXPERIMENTAL ANALYSIS of VORTEX SHEDDING BEHIND D-SHAPED CYLINDER
 
DefenceSeminar
DefenceSeminarDefenceSeminar
DefenceSeminar
 
article-cyclone.pdf
article-cyclone.pdfarticle-cyclone.pdf
article-cyclone.pdf
 
Stress Analysis on Split Ring
Stress Analysis on Split RingStress Analysis on Split Ring
Stress Analysis on Split Ring
 
Final Presentation_Ekramul_Haque_Ehite_04042016
Final Presentation_Ekramul_Haque_Ehite_04042016Final Presentation_Ekramul_Haque_Ehite_04042016
Final Presentation_Ekramul_Haque_Ehite_04042016
 
J012665565
J012665565J012665565
J012665565
 
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...
Generation of Air Swirl through Inlet Poppet Valve Modification and To Enhanc...
 
EME185 Presentation
EME185 PresentationEME185 Presentation
EME185 Presentation
 
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...
An Investigation into the Flow Mechanism of Gas-Solids Flow of Fine and Dusty...
 
projetcs&contributions
projetcs&contributionsprojetcs&contributions
projetcs&contributions
 
Energy Conversion Analysis Webinar
Energy Conversion Analysis WebinarEnergy Conversion Analysis Webinar
Energy Conversion Analysis Webinar
 
Development and design validation of pneumatic tool for stem seal collet fi...
Development and design validation of pneumatic tool for stem seal   collet fi...Development and design validation of pneumatic tool for stem seal   collet fi...
Development and design validation of pneumatic tool for stem seal collet fi...
 
Design, CFD Analysis and Fabrication of Solar Flat Plate Collector
Design, CFD Analysis and Fabrication of Solar Flat Plate CollectorDesign, CFD Analysis and Fabrication of Solar Flat Plate Collector
Design, CFD Analysis and Fabrication of Solar Flat Plate Collector
 
02_AJMS_363_21_compressed.pdf
02_AJMS_363_21_compressed.pdf02_AJMS_363_21_compressed.pdf
02_AJMS_363_21_compressed.pdf
 
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDER
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDERCFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDER
CFD BASED ANALYSIS OF VORTEX SHEDDING IN NEAR WAKE OF HEXAGONAL CYLINDER
 
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...
GEOMETRIC OPTIMIZATION AND MANUFACTURING PROCESS OF SIX CYLINDER DIESEL ENGIN...
 
PhD_Annual_Review_2023.pdf
PhD_Annual_Review_2023.pdfPhD_Annual_Review_2023.pdf
PhD_Annual_Review_2023.pdf
 
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...
EFFECT OF DAM LOCATION ON THE PERFORMANCE CHARACTERISTICS OF TWO -LOBE BEARIN...
 
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension System
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension SystemDesign and Performance Analysis of Mechanical Hydro Pneumatic Suspension System
Design and Performance Analysis of Mechanical Hydro Pneumatic Suspension System
 
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...
04 - Army-MPR and Stevens Collaboration to Design and Build the Smallest Twin...
 

YOUSSEF_IND

  • 1. Vortex Shedding from a Group of Cylinders ENG 3163: BEng Final Year Project Individual work carried by: Youssef Sayed Project Supervisor: Dr. Matteo Carpentieri
  • 2. Problem Statement  Flow around a circular cylinder has been a classic problem in the fluid mechanics field where lots of experiments have been carried on to understand the flow around it.
  • 3. Research Objectives  This project aims to investigate experimentally and discuss theoretically the behaviour of the wake resulting from different cylinder formations: - Side by side - Tandem - Staggered  Optimise the visualisation technique and the recording systems used during the experiments.  Forming a library of video-clips to be added to the existing set of the EnFlo laboratory album.
  • 4. Wake Configuration Wake Configuration has been debated between many engineers: -Williamson (1985) discussed the two types of wake configuration -Landweber (1942) found that all the vortex shedding are mainly inphase -Thomas & Kraus (1964) detected the formation of inphase and antiphase shedding -Bearman & Wadcock (1973) and Quadflieg (1977) found preponderance of the antiphase type of shedding.
  • 5. Side by side Configuration Two main approximations are the diameter of the cylinders which is noted by ‘D’ and the gap width between the cylinders noted by ‘T’
  • 6. Side by side Configuration Three observations have been noted by Sumner (2010) regarding these formed patterns. (a) The single bluff body ( T/D< 0.2) (b) The based flow pattern (0.2< T/D < 2) (c) Parallel vortex pattern ( T/D> 2)
  • 7. Tandem Configuration Two main approximations are the diameter of the cylinders, noted by ‘D’, and the distance between the centre of the cylinders, known as the centre width noted by ‘L’
  • 8. Staggered Configuration Three observations have been noted by Sumner (2010) regarding these formed patterns. Regime Zdravkovich (1987) Zhou & Yiu (2006) Extended Body Regime 1< L/D <1.2-1.8 1< L/D <2 Extended Body Regime 1.2-1.8< L/D <3.4-3.8 2< L/D <5 Extended Body Regime L/D >3.4-3.8 L/D >5
  • 9. Staggered Configuration The staggered configuration is arrangement of two circular cylinders; the geometry of this configuration is set by the P/D dimensionless ratio and the angle of incidence α
  • 10. Staggered Configuration Four Groups identified by Sumner (2010)
  • 11. Experimental Methodology Modification 1. New towing tank filling mechanism
  • 12. Optimising the Recording Mechanism: 1. New flow control device Experimental Methodology Modification
  • 13. Optimising the Recording Mechanism: 2. Introducing the white sheet Experimental Methodology Modification
  • 14. Support Arms (Tandem configuration) Experimental Methodology Modification
  • 15. Results The results were divided between two phases: First phase experiments: – Response from one cylinder • (a) Testing best angle of injection • (b) Effect of Reynolds number • (c) Development of Vortex Street – Response of cylinders arranged in side by side configuration • (a) Effect of Proximity • (b) Increase Reynolds number • (c) Effect of Increasing Reynolds number with proximity Second phase includes: – Response of cylinders arranged in tandem configuration • (a) Effect of Proximity • (b) Effect of Increasing Reynolds number with proximity
  • 16. Phase One Results Results from the response of one cylinder Selected flow options: Injection =180 deg (Immediate Shedding) Reynolds number =185 (Clear Flow)
  • 17. Phase One Results Results from the response of two cylinder (proximity effect) Cylinders =2 Re =185 proximity=4D Cylinders =2 Re =185 proximity=2D Cylinders =2 Re =185 proximity=1D Cylinders =2 Re =185 proximity=0.5D
  • 18. Phase One Results Results from the response of two cylinder (Re number effect) Cylinders =2 Re =320 proximity=1D Cylinders =2 Re =450 proximity=1D Cylinders =2 Re =450 proximity=2D Cylinders =2 Re =320 proximity=2D
  • 19. Phase One Results Results from the response of multiple cylinders (Increase number of cylinders effect) Cylinders =3 Re =185 proximity=1D Cylinders =4 Re =185 proximity=1D Cylinders =5 Re =185 proximity=1D
  • 20. Phase Two Results Results from the response of two cylinders (proximity effect) Dis=1L/D Dis=2L/D Dis=3L/D Dis=3.5L/D Dis=4.5L/D Dis=5.5L/D
  • 21. Phase Two Results Results from the response of two cylinders (proximity effect) Dis=1L/D Dis=3.5L/D Dis=4.5L/D Dis=5.5L/D • Re= 320 • Re= 450
  • 22. Conclusion and Observations The results were divided between two phases: Phase one observations:  Predominance of the antiphase shedding wake configuration proving the theory of Bearman & Wadcock (1973) and Quadflieg (1977).  Proximities tested using two cylinders (side by side configuration) verified the three flow pattern  Intermediate cylinder using odd number of cylinders, showed anti-phase shedding to both sides of the cylinder.  When an even number of bodies were tested, the two cylinders spaced close together showed an anti-phase shedding nature Phase two observations :  The proximities tested verified three regimes and demonstrated values that are closer to Zhou & Yiu (2006)  The co-shedding system recognised by Igrashi (1981) can have either symmetrical or unsymmetrical mixing.
  • 23. Thank you for your attention