BAIL 2006 Book of Abstracts - Institut für Numerische und ...

BAIL 2006 Book of Abstracts - Institut für Numerische und ... BAIL 2006 Book of Abstracts - Institut für Numerische und ...

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N.V. TARASOVA: Full asymptotic analysis of the Navier-Stokes equations in the problems of gas flows over bodies with large Reynolds number ✬ ✫ the application of the Euler equations for incompressible flow outside the boundary layer and the classical equations of the compressible boundary layer near the body surface makes impossible the agreement between both equation systems. To consider the proposed problems from common positions another special dimensionless variables for gas parameters in the Navier-Stokes equations are introduced. These new variables are varied inside the studied flow area usually from 0 to 1 (in other words, they can vary to the value of the order of unit). The main idea to use such special dimensionless variables is that in this case all governing parameters that can be both small and not small are indicated explicitly as the coefficients in the equation system. Among these parameters are M 2 ∞ and ∆T/T0 (∆T is the temperature drop and T0 is the characteristic value of the temperature in the area). It should be noticed that in the hyposonic flows the gravity force can affect significantly the gas flow (in studies of free and induced convection). In term of asymptotic analysis it means that it is necessary to take account of one more parameter, for example 1/Fr (Fr is the Frud number) that can be both small and not small. The full asymptotic analysis is carried out for all mentioned situations on the base of comparison of all parameters mentioned above (M 2 ∞, ∆T/T0, 1/Fr) with the standard small parameter ε in order of magnitude. As a result, the model for gas flow in both areas is formulated and an attempt to construct the procedure of the agreement of the solutions in both areas is made. It should be stressed that the equation systems derived under the assumptions 1) - 4) differ from each other. This model constructed for the cases 2) and 3) possibly can occupy the intermediate place between two classical approaches when a gas is considered as incompressible or compressible one over the whole flow field. The equations describing hyposonic flows (M → 0) with the arbitrary values of the Reynolds number (Re), ∆T/T0 and 1/Fr were derived in [2] from the Navier-Stokes equations on the base of the asymptotic analysis with the Mach number (M) as a small parameter. In this work an attempt to compare the model constructed for cases 2) and 3) with the results obtained in [2] when considered flow with the large Reynolds number was made. References 1. M. Van Dyke. 1962 In: Hypersonic Flow Research (Ed. F.R.Riddell). Academic Press. 2. A.I. Zhmakin, Yu.N. Makarov. 1985 Numerical modelling of hyposonic flows of viscous gas, Dokl. AN SSSR, Mekh. Zh. i Gaza 280 (4), 827–830. [in Russian] Speaker: TARASOVA, N.V. 144 BAIL 2006 2 ✩ ✪

C.H. TAI, C.-Y. CHAO, J.-C. LEONG, Q.-S. HONG: Effects of golf ball dimple configuration on aerodynamics, trajectory, and acoustics ✬ ✫ International Conference: BAIL 2006 Boundary and Interior Layers - Computational & Asymptotic Methods - Effects of golf ball dimple configuration on aerodynamics, trajectory, and acoustics *Chang-Hsien Tai + Chih-Yeh Chao ++ Jik-Chang Leong + Qing-Shan Hong + *Corresponding author Department of Vehicle engineering, National Pingtung University of Science and Technology + Department of Mechanical engineering, National Pingtung University of Science and Technology ++ 1, Hseuh Fu Road, Neipu Hsiang, Pingtung Taiwan, R.O.C. Fax: 886-8-7740398 E-mail: chtai@mail.npust.edu.tw Abstract In many reports about golf ball, including the history of its development, have introduced the standards on golf ball specification. However, there is not a single well-documented solid requirement found for the design of golf ball surface. Not only have a lot of reports discussed the material and structure of a golf ball, but also most of the golf ball manufacturers improve their products by modifying the number of layers beneath the golf ball surface and their materials. Even so, there are relatively very few papers focused on the influence of different concave surface configurations on the aerodynamic characteristics of the golf ball. Furthermore, the noise a golf ball generates in a tournament is very likely to affect the emotion and hence the performance of the golf ball player. For these reasons, this study investigates the performance of a golf ball based on the CFD method with the validation using a wind tunnel. In 1938, Goldstein [1] had proposed an important parameter – the spin ratio. In corporation with different Reynolds numbers, this parameter makes the study of life and drag effects feasible for whirling smooth bodies. In his book, Jorgensen [2] especially emphasized that the main objective of concaved surfaces on a golf ball is to generate small scale turbulence. When flying, this turbulence postpones air separation, reduces the low pressure region trailing the golf ball, and eventually lowers the air drag. Warring [3] used numerical approach to perform a series of studies related to golf ball using Excel spreadsheets. The goal of his paper was to provide guidance for golf ball players and manufacturers so that their golf ball was capable of flying for a longer distance. In the study of acoustics, Singer, et al. [4] calculated the noise level from a source using a hybrid grid system with the help of Lighthill’s acoustics analytic approach. On the other hand, Montavon, et al. [5] combined CFD method and Computational Aeroacoustics Approach (CAA) to simulate noise generation from a cylinder. Using CFX-5 with LES (Large Eddy Simulation) as their turbulence model and Ffowcs-Williams Hawkings formulation, they had successfully shown that their predicted sound levels agreed very well with theoretical ones for Reynolds numbers about 1.4× 10 5 . Figure 1 shows the flow field around a typical golf ball (Case 1). In Case 2, additional dimples are added onto the golf ball considered in Case 1. The orientation of these additional dimples is depicted in Figure 3. It is found, based on Figure 2, that the flow field associated to Case 2 is no longer symmetrical because of the presence of the additional dimples. Figure 3 demonstrates the distribution of lift and drag coefficients of Cases 1 and 2. Clearly, the addition of small dimples increases the drag. This implies that the golf ball in Case 2 suffers more serious drag effect at low trajectory speeds. The lift the golf ball in Case 2 experiences at moderate Reynolds numbers increases so greatly that it becomes greater than that for Case 1. The life force in overall is therefore greater for Case 2 than Case 1. Although the drag imposed on the golf ball is always smaller for Case 1 than for Case 2, the drag in Case 1 is only about 38.5% less than that in Case 2. However, the lift in Case 2 is 103% greater than that in Case 1. This somewhat indicates the lift effect is 2.68 times of the drag effect. The overall performance of the golf ball for Case 2 is much greater than that for Case 1. Therefore, the former golf ball is capable of traveling further, as shown in Figure 4. Speaker: HONG, Q.-S. 145 BAIL 2006 ✩ ✪

C.H. TAI, C.-Y. CHAO, J.-C. LEONG, Q.-S. HONG: Effects <strong>of</strong> golf ball dimple<br />

configuration on aerodynamics, trajectory, and acoustics<br />

✬<br />

✫<br />

International Conference: <strong>BAIL</strong> <strong>2006</strong><br />

Bo<strong>und</strong>ary and Interior Layers<br />

- Computational & Asymptotic Methods -<br />

Effects <strong>of</strong> golf ball dimple configuration on aerodynamics, trajectory, and acoustics<br />

*Chang-Hsien Tai + Chih-Yeh Chao ++ Jik-Chang Leong + Qing-Shan Hong +<br />

*Corresponding author<br />

Department <strong>of</strong> Vehicle engineering, National Pingtung University <strong>of</strong> Science and Technology +<br />

Department <strong>of</strong> Mechanical engineering, National Pingtung University <strong>of</strong> Science and Technology ++<br />

1, Hseuh Fu Road, Neipu Hsiang, Pingtung Taiwan, R.O.C.<br />

Fax: 886-8-7740398 E-mail: chtai@mail.npust.edu.tw<br />

Abstract<br />

In many reports about golf ball, including the<br />

history <strong>of</strong> its development, have introduced the<br />

standards on golf ball specification. However,<br />

there is not a single well-documented solid<br />

requirement fo<strong>und</strong> for the design <strong>of</strong> golf ball<br />

surface. Not only have a lot <strong>of</strong> reports discussed<br />

the material and structure <strong>of</strong> a golf ball, but also<br />

most <strong>of</strong> the golf ball manufacturers improve their<br />

products by modifying the number <strong>of</strong> layers<br />

beneath the golf ball surface and their materials.<br />

Even so, there are relatively very few papers<br />

focused on the influence <strong>of</strong> different concave<br />

surface configurations on the aerodynamic<br />

characteristics <strong>of</strong> the golf ball. Furthermore, the<br />

noise a golf ball generates in a tournament is very<br />

likely to affect the emotion and hence the<br />

performance <strong>of</strong> the golf ball player. For these<br />

reasons, this study investigates the performance <strong>of</strong><br />

a golf ball based on the CFD method with the<br />

validation using a wind tunnel.<br />

In 1938, Goldstein [1] had proposed an<br />

important parameter – the spin ratio. In<br />

corporation with different Reynolds numbers, this<br />

parameter makes the study <strong>of</strong> life and drag effects<br />

feasible for whirling smooth bodies. In his book,<br />

Jorgensen [2] especially emphasized that the main<br />

objective <strong>of</strong> concaved surfaces on a golf ball is to<br />

generate small scale turbulence. When flying, this<br />

turbulence postpones air separation, reduces the<br />

low pressure region trailing the golf ball, and<br />

eventually lowers the air drag. Warring [3] used<br />

numerical approach to perform a series <strong>of</strong> studies<br />

related to golf ball using Excel spreadsheets. The<br />

goal <strong>of</strong> his paper was to provide guidance for golf<br />

ball players and manufacturers so that their golf<br />

ball was capable <strong>of</strong> flying for a longer distance. In<br />

the study <strong>of</strong> acoustics, Singer, et al. [4] calculated<br />

the noise level from a source using a hybrid grid<br />

system with the help <strong>of</strong> Lighthill’s acoustics<br />

analytic approach. On the other hand, Montavon,<br />

et al. [5] combined CFD method and<br />

Computational Aeroacoustics Approach (CAA) to<br />

simulate noise generation from a cylinder. Using<br />

CFX-5 with LES (Large Eddy Simulation) as their<br />

turbulence model and Ffowcs-Williams Hawkings<br />

formulation, they had successfully shown that their<br />

predicted so<strong>und</strong> levels agreed very well with<br />

theoretical ones for Reynolds numbers about 1.4×<br />

10 5 .<br />

Figure 1 shows the flow field aro<strong>und</strong> a typical<br />

golf ball (Case 1). In Case 2, additional dimples<br />

are added onto the golf ball considered in Case 1.<br />

The orientation <strong>of</strong> these additional dimples is<br />

depicted in Figure 3. It is fo<strong>und</strong>, based on Figure 2,<br />

that the flow field associated to Case 2 is no longer<br />

symmetrical because <strong>of</strong> the presence <strong>of</strong> the<br />

additional dimples. Figure 3 demonstrates the<br />

distribution <strong>of</strong> lift and drag coefficients <strong>of</strong> Cases 1<br />

and 2. Clearly, the addition <strong>of</strong> small dimples<br />

increases the drag. This implies that the golf ball in<br />

Case 2 suffers more serious drag effect at low<br />

trajectory speeds. The lift the golf ball in Case 2<br />

experiences at moderate Reynolds numbers<br />

increases so greatly that it becomes greater than<br />

that for Case 1. The life force in overall is<br />

therefore greater for Case 2 than Case 1. Although<br />

the drag imposed on the golf ball is always smaller<br />

for Case 1 than for Case 2, the drag in Case 1 is<br />

only about 38.5% less than that in Case 2.<br />

However, the lift in Case 2 is 103% greater than<br />

that in Case 1. This somewhat indicates the lift<br />

effect is 2.68 times <strong>of</strong> the drag effect. The overall<br />

performance <strong>of</strong> the golf ball for Case 2 is much<br />

greater than that for Case 1. Therefore, the former<br />

golf ball is capable <strong>of</strong> traveling further, as shown<br />

in Figure 4.<br />

Speaker: HONG, Q.-S. 145 <strong>BAIL</strong> <strong>2006</strong><br />

✩<br />

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