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Pressure and Friction Drag II
Hydromechanics VVR090
ppt by Magnus Larson; revised by Rolf L Jan 2014
SYNOPSIS
1. Drag– General Observations
2. Flow Separation
3. Drag Coefficients for Different Shapes
4. Drag Coefficient for sphere in Laminar Flow
5. Vortex Shedding
6. Examples/Problems
7. Lift Force on Bodies
8. Magnus Effect
1. Drag– General Observations I
Inconvenient to separate between pressure and frictional drag.
Total drag force is taken to be the sum of :
• drag in a two-dimensional flow (profile drag)
• drag produced by end effects (induced drag)
Induced drag is related to the lift force.
No lift force no induced drag
tip vortices
Drag – General Observations II
Pressure drag depends on the pressure distribution around the
body and the size of the separation zone.
Large zone of separation large drag force
The location of separation points decisive for the magnitude of the
pressure drag . Such locations are determined by:
• body shape
• body roughness
• flow conditions
2. Flow Separation
streamlined body cylindral body
Boundary layer growth starts in the stagnation point.
In the phase of acceleration the boundary layer is stable, whereas
during deceleration an unfavorable pressure gradient develops that
leads to separation.
Laminar and Turbulent Boundary Layers
Ideal fluid
Laminar conditions
Turbulent conditions
3. Drag Coefficients for Different Shapes
Drag coefficient depends on Re (sphere, disk, streamlined body).
Transition to
turbulent
boundary
layer
Laminar flowLittle variation
with ReNo separation
Flow around Golf Ball
Turbulent boundary layer stronger
than laminar.
=> Smaller zone of separation and
resulting drag force
Flow around Sphere
Flow separation behind
sphere
Flow separation
point
Flow separation point with trip wire
Trip
wire
Cricket ball
Empirical Values for the Drag Coefficient CD I
Empirical Values for the Drag Coefficient CD II
Dolphin drag
Empirical Values for the Drag Coefficient CD III
LotusVehicle
Year and
Model
Cd Area (m2
)
Area (ft2 ) Cd x m2 Cd x ft2
'80 Eclat 0.360 1.830 19.69 0.66 7.09
'95 Elan
S2
0.380 1.709 18.40 0.65 6.99
'91 Elan
SE
0.380 1.709 18.40 0.65 6.99
'80 Esprit 0.330 1.802 19.40 0.59 6.40
'94 Esprit
S4
0.330 1.802 19.40 0.59 6.40
'83 Esprit
Turbo
0.330 1.802 19.40 0.59 6.40
'86 Esprit
Turbo
0.330 1.802 19.40 0.59 6.40
'89 Esprit
Turbo
0.330 1.802 19.40 0.59 6.40
'90 Esprit
Turbo SE
0.330 1.802 19.40 0.59 6.40
Mercedes-Benz Bionic Concept: 0.19
Hummer H2: 0.57
Lotus
4. Drag Coefficient for sphere in Laminar Flow
Stokes derived the drag force for laminar conditions (viscous
forces dominate):
3 oD V d
General formulation of Drag force:
21
2 D D oD F C A V
Equivalence [ eq. 1 and 2] yields:
213
2 o D oV d C A V
George
Stokes
(eq. 1)
(eq. 2)
(eq. 3)
Cross-sectional area:
2
4
dA
Solve for drag coefficient:
24 24
Re
D
o
CV d
Stokes equation valid for Re < 0.1.
Re 10 weak separation
Re 1000 fully developed separation zone
5. Vortex Shedding
Under certain conditions vortices are generated from the
edges of a body in a flow.
Von Karman’s vortex street
Theodore Von
Karman
Vortex street behind a cylinder
Vortices at Aleutian Island
If 6 < Re < 5000, regular vortex sheeding may occur at a
frequency n determined by Strouhal’s number:
o
ndS
V
(S = 0.21 over a wide range of Re)
Vincent Strouhal
Periodic vortex shedding may lead to transversal forces on
structures (e.g., pipes, chimneys, bridges) resulting in vibration
and possible structural damages.
If is close to the natural frequency of the structure, large effects
are expected.
Strouhals Number as a Function of Re
Fully developed
turbulence, no regular
vortex sheddingData for cylinder
6. Examples / problems
Example I: Vortex Shedding from Antenna Stand
30 m
0.3 m
What is the frequency of the vortices shed?
wind
35 m/s
Standard atmosphere
(101 kPa, 20 deg)
Example II: Vortex Shedding from Telegraph Wires
V = 10 m/sWires
diameter = 2 mm
What is the frequency of the vortices shed?
Examples of Drag Force Calculation
III ) parachute jumping
IV ) sedimentation of particle
V ) popcorn popper
Basic equation for drag force:
21
2 D oD C AV
Where:
CD is obtained from empirical studies
A is the projected area on a plane
perpendicular to the flow direction
Example III: Parachute Jumping
FG
FDTerminal speed of a person jumping with a
parachute?
Assumed data:
M = 100 kg
air = 1.2 kg/m3
D = 7 m
Example IV: Particle Sedimentation
Sediment particle in water – what is the
terminal speed?
Newton-Stokes law of sedimentation
(laminar flow)
FG
FB FD
Examples of
settling tanks
Example V: Popcorn Popper
Design the popcorn popper
Unpopped corn:
0.15 g/kernel
6 mm diameter
Popped corn:
18 mm diameter
Allowable air speed produced by the fan?
Fan
Heating
coil
Ferrybridge Cooling Towers
Three towers collapsed (November 1965) because:
• underestimated wind design conditions
• interaction between towers not considered
Tacoma Bridge
Built 1940
Span: 2,800 ft (850 m)
Plate-girder deck: 8 ft (2.4 m)
Wind-induced vibrations
caused oscillations of the
deck with eventual collapse.
7. Lift Force on Bodies
Important in design of:
• airplane
• pipelines (e.g., on the seafloor)
• pumps and turbines
Flow and pressure
distribution around and airfoil
Principles of Flight
Horizontal and vertical force
balance for design
FL = FG
FD = FP
21
2L L oF C A V
Lift force:Gliding angle:
tan D
L
C
C
Lift Coefficient CL
CL for typical airfoil sections versus
angle of attack
Stall speed
Tip Vortices (Induced Drag) I
Tip Vortices (Induced Drag) II
CD and CL for different wing aspect ratios
8. Magnus Effect
Heinrich
Gustav
Magnus
Net force occurs when a sphere or cylinder in a
moving fluid is rotating
Top of cylinder: velocities of the moving fluid and the
rotating ball enhance each other low pressure
Bottom of cylinder: velocities of the moving fluid and the
rotating ball counteract each other high pressure
Pressure difference net force
Popular explanation
Importance of Magnus Effect in Sports I
Golf (hook, slice)
Soccer
(banana
shoot)
Table tennis
and tennis
(topspin, slice)
Lateral deflection
of baseball
Importance of Magnus Effect in Sports II
Spinning baseball
(curveball)
Asymmetric boundary layer
separation
Ship Propulsion
Alcyone
(Cousteau)
Buckau
Anton Flettner