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Procedia Engineering 72 (2014) 780 – 785
The 2014 conference of the International Sports Engineering Association
The influence of golf ball dimples on aerodynamic characteristics
Takeshi Naruoa, *, Taketo Mizotab
a
b
Mizuno Corporation, 1-12-35, Nanko-Kita, Suminoe-ku,Osaka, 559-8510, Japan
Fukuoka Institute of Technology, 3-30-1, Wajiro-higashi, Higashi-ku, Fukuoka, 811-0295, Japan
Abstract
Aerodynamic forces act on a golf ball during flight. For that purpose in order to develop a golf ball with high performance, it is
important to analyze aerodynamic characteristics of the golf ball. On the other hand, dimple pattern of a golf ball is complicate
and the influence of dimples hasn’t been investigated in detail. Therefore the influence of golf ball dimples on aerodynamic
characteristics was investigated using a wind tunnel and rotating device. Some golf balls whose dimples have different depths
were measured. As a result, it was found that the shallower the dimple was, the larger the lift coefficient was. However, when
the depth of the dimples was much shallower, the lift coefficient was extremely-little on the slow velocity, i.e. under 30m/s.
When the golf ball trajectory which was launched with a driver was calculated under various initial conditions, the ball velocity
became under 30 m/s over the vertex of the trajectory in many cases, including professional male golfers and female golfers.
Therefore, if the lift coefficient of the velocity of 30m/s becomes smaller, distances will become shorter. Dimple patterns that
had a high lift coefficient at all velocities was researched. As a result, it was found that a golf ball with a dimple pattern that
has extremely small dimples between large shallow dimples has a high lift coefficient at all velocities, including under 30m/s.
In order to investigate the cause of the results, a flow visualization experiment was conducted. Visualization of flow around a
golf ball was conducted by generating smoke. Moreover pictures of flow were taken by high-speed video and analyzed by PIV
(Particle Image Velocimetry). As a result, there was the difference in the streamline distribution between golf balls.
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© 2014
2014 The
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Open access
Selection
Research,
Sheffield
Hallam
University.
Selection and
andpeer-review
peer-reviewunder
underresponsibility
responsibilityofofthe
theCentre
Centrefor
forSports
SportsEngineering
Engineering
Research,
Sheffield
Hallam
University
Keywords: aerodynamics; wind tunnel; golf ball; PIV
* Corresponding author. Tel.: +81-6-6614-8291; fax:+81-6-6614-8481
E-mail address: tnaruo@mizuno.co.jp
1877-7058 © 2014 Published by Elsevier Ltd. Open access under CC BY-NC-ND license.
Selection and peer-review under responsibility of the Centre for Sports Engineering Research, Sheffield Hallam University
doi:10.1016/j.proeng.2014.06.132
Takeshi Naruo and Taketo Mizota / Procedia Engineering 72 (2014) 780 – 785
781
1. Introduction
The largest flight-distance of a golf ball reached 300m by a driver, and the golf ball flew for 6 seconds. During
flight, aerodynamic forces act on the golf ball. Mizota and Naruo (2002) developed a wind tunnel and a ballrotating device that provides flow velocity and spin to the golf balls that match actual flight conditions. The golf
ball velocity and spin rate were changed variously and the aerodynamic force coefficients C D , C L and C M were
measured under many conditions. As a result, aerodynamic force coefficients were dependent on Reynolds
Number Re changes, and could be put in order only by spin rate parameters S P .
On the other hand, a golf ball has many hollows in the surface, called dimples. The arrangement of the dimples,
structure, size, depth and form are various. Although it is said that influence for the aerodynamic forces
characteristic is large, there is no research and not many reports. Sajima etc. (2006) considered the influence of the
depth using CFD. In the study, the influence of dimples was systematized and investigated using the wind tunnel
and the ball-rotation device. Consequently, it was found that the influence of the depth of the dimples was large,
and the shallower it was made, the more the lift coefficient went up and it gained a high trajectory.
Furthermore, when it was made shallow exceeding a certain threshold, it became clear that the lift coefficient
declined greatly in the low-speed region of 30 m/s or less. As a result of the trajectory analysis, on the condition of
a male pro golfer, a female pro golfer or an ordinary male amateur with a driver, the golf ball velocity becomes
30m/s or less when the golf ball flies in the second half of the trajectory which passes the vertex. Thereby, if a lift
coefficient declines greatly in the low-speed region of 30 or less m/s, flight-distance will become shorter. A dimple
design which realizes an antithesis that does not have the fall of a lift coefficient in a low-speed range but has high
lift coefficient in a high-speed range of 30m/s or more is desired.
2. Wind tunnel test methods
With the ball-rotation device installed into the wind tunnel wind, high-speed rotation of the golf ball was carried
out, and aerodynamic forces were measured by the three-dimensional load cell arranged under the ball-rotation
device. In order to rotate a golf ball, a miniature bearing is placed in the golf ball.
In order for the tension of piano wires to prevent miniature bearing damage, it lets the thin inner tube pass inside
the shaft. The piano wires which let the golf ball pass are attached to a frame so that a golf ball may be arranged in
the center of the frame, as shown in Fig.1. High-speed rotation is carried out by blowing against a golf ball with jet
air. By measuring the number of revolutions within a wind tunnel flow, the aerodynamic force coefficients
corresponding to the spin rate parameter (circumference against flow peripheral velocity) which changes one after
another was measured.
Fig.1. A wind tunnel and rotating device
Fig.2. Transmissive image of a golf ball for experiment
As shown in Fig.2, in order to maintain a dynamic balance, a set bolt was put into surface of golf ball from three
directions, and respective positions were adjusted. By this adjustment, even if it rotated at the high speed of 200
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Takeshi Naruo and Taketo Mizota / Procedia Engineering 72 (2014) 780 – 785
rps, it became measurable without vibration. There were six kinds of flow velocities of the wind tunnel, 44 m/s, 40
m/s, 35 m/s, 30 m/s, 28 m/s, and 25 m/s. In a constant flow velocity, aerodynamic forces were measured
continuously when the number of revolutions was set at 200 rps and decreased after that.
3. Influence of dimple on aerodynamic forces
3.1. Influence of dimple depth
The golf balls for the study are shown in Table 1. Dimple shape and the arrangement of Golf Ball A and Golf
Ball B are the same, and only the depth is different. The lift coefficient obtained from the wind tunnel test is shown
in Fig.3.
Table 1. Golf balls for study
Number of
dimples
Diameter of large
dimples (mm)
Depth of large
dimples (mm)
Golf Ball A
366
4.27
0.158
Golf Ball B
366
4.27
0.123
CL
CL
S㹎
S㹎
(a) Golf Ball A
(b) Golf Ball B
Fig. 3. Results of wind tunnel experiment
Fig. 4. Results of trajectory analysis (a) Trajectory (upper) ; (b) Velocity (lower)
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Takeshi Naruo and Taketo Mizota / Procedia Engineering 72 (2014) 780 – 785
In a flow velocity of 35 m/s or more, there is almost no difference between some flow velocities, i.e. the
Reynolds number. Also, Golf Ball B with a shallow dimple has a larger lift coefficient throughout the spin
parameter compared to Golf Ball A. However, when it becomes less than 30 m/s, although flow velocity
dependences have not appeared in Golf Ball A, they have appeared in Golf Ball B significantly
Trajectories of Golf Ball A and Golf Ball B were analyzed based on Mizota and Naruo (2002 and 2004). The
typical data of the driver shot of male professional golfer was used for the initial condition immediately after
impact of the golf ball. The trajectory analysis result is shown in Fig.4. It was also found that in cases of even
male pro golfers, ball velocity becomes less than 30 m/s soon after the golf ball passes over the vertex. Therefore,
it turns out that aerodynamic characteristics of the velocity of less than 30m/s, is important. Comparing Golf Ball
A and Golf Ball B, Golf Ball B with a higher lift coefficient at 30 m/s or more has a higher trajectory after impact,
but after passing the vertex, ball velocity becomes less than 30 m/s and the golf ball falls rapidly. In order to
lengthen flight-distance, it was discovered that the lift coefficient of less than 30 m/s is important.
3.2. Effect of tiny dimples
In our other study, it turned out that lift coefficients raise when the depth of dimples is shallow, the number of
dimples is lessened, dimples are enlarged, or the share of dimples on all surface is lessened. Also, velocity
dependency appears in the low-speed region of 30 m/s or less, and a lift coefficient falls.
In order to lose the fall of a lift coefficient in a low-velocity range, realizing high lift coefficients on high-speed
conditions, tiny dimples are arranged between large dimples. The dimple arrangement is shown in Fig. 5(a). In
order to compare the aerodynamic characteristics, the golf ball which lost only tiny dimples was also created. (Fig.
5 (b)) The specifications of the dimple are shown in Table 2. The lift coefficient obtained from the wind tunnel test
of two golf balls is shown in Fig.6. Although, the fall of a lift coefficient clearly appears on the low condition of 30
m/s; as for Golf Ball D, the fall in the case of Golf Ball C almost does not appear.
Flight trajectory analyses for both golf balls were conducted under the same conditions as Capture 3-1. The
result is shown in Fig.7. The difference in height after passing the vertex mentioned above appeared significantly,
and flight-distance of Golf Ball C became larger compared to Golf Ball D.
(a) Golf Ball C
(b) Golf Ball D
Fig. 5. Golf balls for study
Table 2. Golf balls for study
Number of
dimples
Diameter of large
dimples (mm)
Depth of large
dimples (mm)
Diameter of tiny
dimples (mm)
Depth of tiny
dimples (mm)
Golf Ball C
278 & 252
4.81
0.148
1.24
0.191
Golf Ball D
278
4.81
0.148
㸫
㸫
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Takeshi Naruo and Taketo Mizota / Procedia Engineering 72 (2014) 780 – 785
(a) Golf Ball C
Fig.6 Results of wind tunnel experiment
(b) Golf Ball D
Fig.7. Results of trajectory analysis
4. Visualization Experiment
4.1. Fuming device
In order to investigate how differences of dimples affect a flow, a visualization experiment was conducted, and
peeling point and status of wake flows were observed. For gas visualization methods, although there were smoke
wire methods, spark tracing methods, suspension methods, etc., where a ball is rotated, smoke wire methods were
adopted because of easy experiment.
However conventional smoke wire methods could be used at a wind velocity of 0.02̚10 [m/s]. (Kim, 2012)
Then, the device to allow enough smoke to flow at a fast velocity was developed by stretching a wire in the upper
stream of the flow. Piano wire was stretched on the frame of a cuboid, and some stainless wires were stretched
between the piano wires. As liquid paraffin sank into a knit lump of stainless wires, it was able to be made to a full
fume, so that a visualization experiment was able to be performed while also in the airflow of the wind velocity of
40 m/s. The frame, i.e. the fuming device, was installed in the wind tunnel.
4.2. Visualization Experiment Method and Result
The visualization experiment was conducted on Golf Ball E and Golf Ball C by flow velocities of 25 m/s, 28
m/s, 30 m/s, and 40 m/s. Golf Ball E is a ball with which the lift coefficient declines greatly by less than 30 m/s,
like Golf Ball B. A similar ball-rotating device as Capture 2 was used. A high velocity revolution was carried out
with the air jet, and the number of revolutions to decrease was measured with a tachometer. Smoke was generated
at the number of revolutions set to S P = 0.1 and S P = 0.2, respectively, and took a photograph of 20,000 frames
per second using high-speed video (Fastcam SA5 made by PHOTORON). The example of the photoed image is
Takeshi Naruo and Taketo Mizota / Procedia Engineering 72 (2014) 780 – 785
shown in Fig.8. In the case of 40 m/s, it was confirmed that the flow was greatly bent downward in the
downstream. In the case of 25 m/s, there was a low level of downstream turn that can be understood as a difference
in lift. In ball comparison, a change in the direction of flow in the downstream of Golf Ball E appeared from
moment to moment at the low velocity. A change almost did not appear in the case of Golf Ball C.
Particle Imaging Velocimetry (PIV) was conducted using Image Tracker (made by DEJIMO). For a certain
period of time (3ms), 60 frames were taken out, and streamline distribution was analyzed. Directions of the flow
mentioned above can be conformed clearly. Moreover, in order to examine a change, some 60-frame sets were
taken out and analyzed in the same experiment. Although Golf Ball C is carrying out almost the same streamline
distribution as the case of the 60 frames, it turns out that the streamline distribution changes in the case of Golf
Ball E. This change makes the flow unstable and it is thought that it makes the lift lower.
(a) 25m/s, S P = 0.1
Fig. 8. Streamline distribution
(b) 40m/s, S P = 0.2
5. Consideration
As a result of the wind tunnel experiment results, in a high flow velocity of 35 m/s or more, a golf ball with
shallower dimples has a higher lift coefficient. However, when exceeding a threshold, if it becomes too shallow, a
lift coefficient will decline greatly at the low speed of less than 30 m/s, and the Reynolds number dependents will
appear. The same effect as when making a shallow dimple is seen by enlarging the dimple and lessening the
number. By arranging tiny dimples in the crevices between large dimples, it is able to keep a high lift coefficient.
In particular, also in the low speeds of less than 30 m/s, it hardly changes, and a lift coefficient of the Reynolds
number dependence is almost not shown.
By the smoke wire method using the steel wires arranged in the upper stream of the flow, it succeeded in flow
visualizations to 40 m/s. PIV was carried out analyzing the visualized high-speed video. As a result, the difference
in flow velocity and the difference between golf balls showed differences in the streamline distribution. In the golf
ball to which a lift coefficient declines greatly in a low-speed range, there is momentarily a change of the
streamline distribution and it was found that it is unstable.
References
Mizota, T., Naruo, T., Shimozono, H., Zdravkovich, M., Sato, F., 2002. 3-Dimensional Trajectory Analysis of Golf Balls, Science and Golf ϫ,
E &F.N.Spon, London, pp. 349-358.
Naruo, T., Mizota, T., 2004. Trajetory Analysis and Optimum Trajectory of a Golfball, Engineerig of Sport 5, Blackwell Science Ltd., Oxford,
pp. 432-439.
Sajima, T., Yamaguchi, T., Yabu, M., Tsunoda, M., 2006. The Aerodynamic Influence of Dimple Design on Flying Golf Ball, The Engineerig
of Sport 6, Springer Science+Business Media, LLC, pp. 143-148.
Kim, H., Onuki, M., Kishibe, S., Tatani,R., Sakaue, S., Arai,T., 2013. Visualization and Measurement of Separation Positions aruound Rotating
Dimpled Ball, The Engineering of Sport 9, SciVerse ScienceDirect, Elsevier Ltd., pp. 194-199.
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