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Aerodynamic design of a 300kW horizontal axis wind turbine for province of Semnan[

Aerodynamic design of a 300kW horizontal axis wind turbine for province of Semnan[
Aerodynamic design of a 300kW horizontal axis wind turbine for province of Semnan[

Aerodynamic design of a 300kW horizontal axis wind turbine for province of Semnan

A.Sedaghat ?,M.Mirhosseini

Department of Mechanical Engineering,Isfahan University of Technology,Isfahan 84156-83111,Iran

a r t i c l e i n f o Article history:

Available online 12April 2012Keywords:

Horizontal axis wind turbine (HAWT)Aerodynamic design BEM theory Chord Twist

a b s t r a c t

In this research,Blade Element Momentum theory (BEM)is used to design a HAWT blade for a 300kW horizontal axis wind turbine.The airfoil is RIS?-A1-18,produced by RIS?National Laboratory,Denmark.Desirable properties of this airfoil are related to enhancement of aerodynamic and structure interactions.Design parameters considered here are wind tip speed ratio,nominal wind speed and diameter of rotor.The nominal wind speed was obtained from statistical analysis of wind speed data from province of Semnan in Iran.BEM is used for obtaining maximum lift to drag ratio for each elemental constitution of the blade.Obtaining chord and twist distribution at assumed tip speed ratio of blade,the aerodynamic shape of the blade in every part is speci?ed which correspond to maximum accessible power coef?cient.The design parameters are trust coef?cients,power coef?cient,angle of attack,angle of relative wind,drag and lift coef?cients,axial and angular induction factors.The blade design distributions are presented versus rotor radius for BEM results.The blade shape then can be modi?ed for ease of manufacturing,structural concerns,and to reduce costs.

ó2012Elsevier Ltd.All rights reserved.

1.Introduction

In consideration of the pertinent policies such as geographical position,environmental protection and government’s tax allow-ance,many countries proffered huge funds on technology of wind-power electricity generation and so it developed very fast than compare with technology of thermal power.Utilizing of wind energy has been progressed by more than 50countries in the whole world considerably [1].Wind turbines have exhibited their ability to sustain whereas wind energy is a clean,raw material-costless,favorable renewable energy.Wind turbine are classi?ed into two con?gurations based on their rotational rotor axis with respect to the ground:the older generation,lower-power vertical axis (e.g.Savonius and Darrieus rotor)and the higher power,horizontal-axis at wide commercial deployment (e.g.AWE series 54-900,52-750,Vestas series v39,and v66,and Nordtank-300).The potential energy of wind is estimated to be about 6500MW in Iran [2].Germany,for example,produced some 4400MW of electricity from wind;while,Iran with a similar level of available wind power produces approximately 100MW according to recent news from the ministry of power in Iran [3].There are abundant wind resources freely available in Northern part of Iran.Manjil,Binalood,and Semnan areas are located in the northern part of the country.There are 21installed wind turbines in Manjil,1with 500kW,5with 550kW and 15with 300kW capacities plus 27more wind turbines were installed by 1999in Manjil,Roodbar and Harzevil and recent employment of 28.4MW in Binalood [3–5].Semnan province,as shown in Fig.1,with 5.6%of the whole area of Iran is the sixth big province in the country.Semnan province area is 95,815km 2.Semnan is located between N34°400–N37°100latitude and E51°590–E57°40longitude [4].

The province of Semnan is bordered from east by the province of Khorasan razavi,from north,Northern Khorasan,Mazandaran and Golestan provinces,from south,Yazd and Esfahan provinces,west,Tehran and Qom provinces.The center of province,Semnan is located at 228km from Tehran and the distance from interna-tional waters of Persian Gulf and Caspian Sea in turn is 1600and 200km.This province includes 5townships,13districts,18cities and 29villages.According to the latest statistics in 2001,the pop-ulation of the province is estimated to be 558,000that 73.5%were in urban area and 26.5%were rural dwellers [7].In general,the dominant prevailing wind in the area is blowing from the north-west to the southeast and is called Tooraneh.Also other winds in the province called Shahriari,Kavir and Khorasan winds,blow from west,south and east to west in different seasons of the year,respectively [8,9].Detailed statistical study of wind at 10m,30m and 40m height in Semnan province is presented in [4].2.Aerodynamic of a horizontal axis wind turbine (HAWT)In the development of modern commercial wind turbines,the size has contiguously increased to the latest multi-MW turbines such as the wind farm shown in Fig.2.Generally,the two

0196-8904/$-see front matter ó2012Elsevier Ltd.All rights reserved.https://www.wendangku.net/doc/0411183298.html,/10.1016/j.enconman.2012.01.033

Corresponding author.

E-mail address:sedaghat@cc.iut.ac.ir (A.Sedaghat).

Fig.1.The location of Semnan province in the map of Iran[6].

Fig.2.Group of HAWTs in a wind farm in UK[10].

fundamental objectives of the design of a HAWT turbine are

maximize its annual energy production(AEP)and to minimize

the cost of energy(COE)produced[11–13].Recently,focus has

been intensi?ed on designing wind turbine rotors for maximum

aerodynamic performance[14–22].According to particularly chal-

lenges and dif?culties to achieve a good ef?ciency and thus

obtaining better economical performance,any improvement

the aerodynamic design of wind turbines infers a signi?cant bene-

that increase.Aerodynamic ef?ciency of wind turbines extre-

mely depends on the performance of the rotor blade,the airfoil

section,and the design form.The theoretical maximum for the

Fig.4.Actuator disk modelling of a wind turbine in a stream tube.

r U

?U ??????????????????????????????????????????C e1t2=k T

C 2

e1t1=k T

à1

!v u u t e6T

For Haddadeh region in province of Semnan in Iran,k =1.6,c =6.52,and the annual mean wind speed and the corresponding rated wind speed is calculated to be 5.85and 8at a height of 40m,respectively [4].

2.2.Rotor speci?cation for HAWTs

The design of the blade requires a great number of design vari-ables parameters to control rotor shape and airfoil characteristics including:the number of blade B ,the rotor diameter D ,the section airfoil lift to drag ratio that depend on the angle of attack a ,and the chord length c ,and twist angle h t at each section of blade.In com-mercial HAWTs,it is normally chosen three blades (B =3).If fewer than three blades are selected,there will be a number of structural problems that must be considered in the hub design.

To determine rotor diameter from Eq.(1),the maximum acces-sible power coef?cient,C p ,max ,is sought.According to the type of application,we need an optimum wind tip speed ratio,de?ned as the rotational speed of blade tip,R X ,to the wind speed,U ;i.e.k ?R X =U .For a water pumping windmill,for which greater torque is needed,we use 1

In this work,the maximum accessible power coef?cient,C p ,max ,and the corresponding optimum value of k opt is calculated from the empirical relation [23]:

C p ;max

?16 k 1:32tk à820àá2B "

#à1àe0:57Tk 2

Cl Cd k t12B

àáe7T

Fig.3shows a group of C p –k curves for a three bladed HAWT

In order to specify the airfoil type,the maximum lift-to-drag ra-tio is criterion with other dynamical,roughness sensitivity,and stall behavior of airfoil for the class of wind power considered.Fun-damentally,the determination of the rotor size depends on the re-quired energy and blown mean wind speed.As relative wind speed is the resultant of the stream wind speed,blade section speed and rotor induced ?ow.Lift force is the main force for operating the wind turbine to produce useful power.Airfoils for HAWT are often designed to be used at low attack angle,where the drag coef?cient is usually much lower than the lift coef?cient.Especially,at blade

Fig.5.Annular control volumes for calculating wake rotation.

Fig.6.Annular control volumes for calculating wake rotation.

tip airfoils with high lift to drag ratio,low roughness sensitivity, low noise character should be selected to insure the nearest opti-mum aerodynamic performance.Grif?ths[24]showed that the output power is greatly affected by the airfoil lift-to-drag ratio.A general aviation airfoil shape is NACA series,and dedicated airfoil shapes used in modern wind turbines are:S8series developed by National Renewable Energy Laboratory(NREL)in USA,FFA-W ser-ies developed by FOI in Sweden,RIS?-A1series developed by RIS?in Denmark,DU series developed by Delft University of Technology in Netherlands.It has been found in some applications that more than one airfoil shape can be used for the wind turbine blade de-sign,but there will be bending between these airfoils which may add to uncertainties in the design process.

In this project,the RIS?type airfoils are used[25].In this class of airfoils,the different families of modern airfoils applied in wind turbines,are veri?ed that with regarding veri?cation of criteria re-late to design of wind turbines,the airfoils RIS?-A1-18,FFA-W3-301,FFA-W3-241,DU93-W-210,were proper choices from which RIS?-A1-18is selected for the300kW HAWT in this study[25]. The experimental results of RIS?-A1are related to open test part of VELUX wind tunnel measurements with1%turbulence.Details of these tests and measurement instruments are given in[26].Also the tests were carried out in the Reynolds number equal to 1.6?106.A generalized analysis on manufacturing,industrializa-tion,and costs shows that the obtained chord length and twist an-gle from the theoretical analysis should be modi?ed[27].Whereas the chord length and twist angle of the wind turbines design are not linear,one procedure for this goal(e.g.simpli?cation in CNC machining for blade’s mold manufacturers)is applying?tted linear relationship on the chord length and twist angle curves separately, yet not considered here.

From the experimental data for the RIS?-A-18airfoil[25],lift coef?cient against angle of attack,i.e.Cl–a,and drag coef?cient against angle of attack,i.e.Cd–a,is used and approximated by a lin-ear equation for the lift coef?cient and a quadratic equation for the drag coef?cient versus the angle of attack.The maximum lift to drag ratio(Cl/Cd)is calculated to be(Cl/Cd)max=167at the angle of attack of a=7°for RIS?-A1-18airfoil.From Fig.3for the RIS?-A-18aerofoil with the maximum lift to drag ratio equals of 167,the optimum tip speed ratio is obtained to be k opt=10for the corresponding maximum power coef?cient of C p,max=0.51. Assuming a mechanical-electrical ef?ciency of g=0.9and adopting the rated wind speed of U?8m from the statistical analysis of wind data at Semnan province[4],the Rotor diameter is calculated from Eq.(1)to be equals to D=54m.To obtain an optimum blade shape as a guide,i.e.chord length and twist angle distribution along the blade,the Blade Element Momentum(BEM)theory is employed discussed next[23].The blade shape then can be modi-

90 A.Sedaghat,M.Mirhosseini/Energy Conversion and Management63(2012)87–94

?ed for ease of manufacturing,structural concerns,and to reduce costs.

2.3.Rotor design using BEM theory

The primitive blade shape is determined using an optimum shape blade considering wake rotating.Ultimate blade shape and its performance are speci?ed with iterative relations and including drag,tip losses and ease of manufacturing.It is also worth empha-sizing that with more accurate aerodynamic coef?cients at high at-tack angles,the more accurate design and performance prediction can be obtained.But the aerodynamic coef?cients of a rotating air-foil are different from the ones of a linear moving airfoil at stall conditions.

Considering the rotor as an actuator disk which its effects are a sudden drop in pressure and assuming constant speed at the rotor [23],the linear momentum theory is used for air?ow through a one dimensional tube as shown in Fig.4.

From Betz theory,an ideal wind turbine reduces wind speed to two third of the freestream value[23].Since the wind turbine pro-duces a useful torque for generating power,the conservation of moment of momentum must be satis?ed by employing a wake rotation downstream of the wind turbine in some annular control volumes as shown in Fig.5.

In actuator disk theory,friction drag is ignored which is not realistic.In order to modify this shortcoming[23],blade element theory is considered to incorporate the effects of drag force exerted on each elemental constitution of blade as shown in Fig.6.

Adopting the procedure discussed in Manwell[23],one may calculate the power coef?cient through an iterative method to the following form:

C p?8=k2

Z k

k h

F k3

r

ae1àaT1àeCd=ClTcot h

? d k re8T

F is tip loss correction factor,a is axial induction factor, a is angular induction factor,k r?r X=U is the local speed ratio for an element of blade at radial distance of r.The element dimension is c as the local chord length and dr as the width of element.The drag to lift ratio eCd=ClTcorresponds to the local airfoil section.

2.4.Rotor control for HAWTs

In high wind speeds,it is noteworthy to be able to control and limit the rotational mechanical power.The power limitation may be done either by stall control,pitch control or active stall control. Pitch control system in wind turbines have become the more appli-cable type of installed wind turbines in recent years.For low wind speeds,the speed controller can continuously adjust the speed of

A.Sedaghat,M.Mirhosseini/Energy Conversion and Management63(2012)87–9491

the rotor to maintain the tip speed ratio constant to produce the maximum power coef?cient,and to improve the ef?ciency of the turbine.For higher wind speeds however pitch angle regulation is required to keep the rotational speed constant.Small changes in pitch angle can reduce considerably the power output.There-fore,the purpose of the pitch angle control may be expressed as [28,29]:

1.Optimizing the power output of the wind turbine.

3.Results and discussion

Fig.7a shows that chord length distribution from the BEM anal-ysis.The maximum chord length calculated to be 2.6m at nearly 10%of blade length from the blade root to the value of nearly 0.3m at tip.From the practical point of view,higher chord length near the root contribute less to the power gained from wind turbine and therefore it can be modi?ed to reduce material weights and costs and also provide ease of manufacturing [30–33].Fig.7b shows the twist angle distribution across the blade length varying from 38°in root to nearly 0°near tip of blade.The twist angle var-iation along the rotor blade maintains the optimum sectional angle of attack for producing the maximum lift to drag ratio at each section.

In Fig.8a,the angle of relative wind is varying from 43°in root to 3°at tip producing the much desirable angle of attack value of 7°as shown in Fig.8b.The angle of attack,a ,is constant for the full length of the blade except from 90%of the blade length near to tip that rapidly decreases to values of 6.2°due to tip losses.Tip losses are due to tip vortexes generated at the tip of blades.The undesirable effects of tip losses may be reduced by incorporating new technologies developed in aviation industry [34]such as wingtips implemented in ?xed wing aircrafts or reshaping tip blades in aircraft propellers.

Fig.9a demonstrates that for any angle of attack,Cl is almost constant to the value of 1.11except at the tip which it drops to the value of 1.05.Drag coef?cient distribution is shown in Fig.9b which exhibit a constant value of 0.0069everywhere.This provides a lift to drag ratio of 161nearly for 90%of the length of blade a very desirable value for wind turbine blades.For large HAWT blades,the Fig.13.Monthly power density of Haddadeh at 40m.

92 A.Sedaghat,M.Mirhosseini /Energy Conversion and Management 63(2012)87–94

comprehensive methods such as experimental measurements [33]and/or computational ?uid dynamics (CFD)techniques [35].

Fig.11a shows the local thrust coef?cient,C t ,which is almost equals to the constant value of nearly 0.88which gradually de-creases to about 0.84near in both the root and the tip of blade.Fig.11b shows the power coef?cient for the rotor blade which pos-sess its maximum (C p =1.1)near tip at 90%of the blade length.The variation of power coef?cient across the rotor blade is nearly a lin-ear function except a small margin near the tip of blade.An opti-mum power distribution along the blade may concern with reducing blade’s loads towards the tip of blade.This accomplish in some designs by using variable airfoil sections from root to tip of blade to reduce the maximum lift coef?cient Cl max at sections near the tip of blade [31].

In Fig.12,the characteristic performance of the designed blade in terms of the power coef?cient C p against tip speed ratios k is shown.It is observed that C p increases to its maximum (0.51)with k up to its optimum value of 10,and then it decreases at higher tip speed ratio values.

Thus,the predicted aerodynamic characteristics of the designed 300kW HAWT is achieved according to the initial achievable opti-mum value of C p max =0.51at k =10.The monthly power density of wind at Haddadeh calculated from annual wind data [7]is pre-sented in Fig.13.The available 10minutely measured wind data at the heights of 10m,30m,and 40m were provided by the Ira-nian renewable energy organisation (SUNA)[36]for the period of 12months.

Fig.14also compares the results from the measured wind data by the Iranian renewable energy organisation (SUNA)[36]and our Weibull distribution which shows power density at height of 40m is relatively good around 300W/m 2for the class of wind turbine designed here.4.Conclusion

There are abundant high quality wind resources available in Iran;however,the growth of wind turbine industry has been very slow in Iran.This work attempts to address some issues and to pre-liminary design a site speci?c 300kW wind turbine based on man-ufacturing and economical capabilities and also power demands in the province of Semnan.The positive attitudes in power organiza-tion in Iran for moving towards clean and renewable energies have encouraged this type of research in several universities and private organizations in Iran.This as yet requires incentives from European and other developed countries to support research in renewable energies in developing countries both economically and technolog-ically to assist moving faster towards the world of carbon free.To withstand against increasing CO 2emission into our environment

and global warming,imminent international efforts and collabora-tions are required to further develop and enhance use of wind en-ergy and other renewable resources.

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从实践的角度探讨在日语教学中多媒体课件的应用

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第10课 日本的季节 日本的一年有春、夏、秋、冬四个季节。 3月、4月和5月这三个月是春季。春季是个暖和的好季节。桃花、樱花等花儿开得很美。人们在4月去赏花。 6月到8月是夏季。夏季非常闷热。人们去北海道旅游。7月和8月是暑假,年轻人去海边或山上。也有很多人去攀登富士山。富士山是日本最高的山。 9月、10月和11月这3个月是秋季。秋季很凉爽,晴朗的日子较多。苹果、桔子等许多水果在这个季节成熟。 12月到2月是冬季。日本的南部冬天不太冷。北部非常冷,下很多雪。去年冬天东京也很冷。今年大概不会那么冷吧。如果冷的话,人们就使用暖气炉。 第12课 乡下 我爷爷住哎乡下。今天,我要去爷爷家。早上天很阴,但中午天空开始变亮,天转好了。我急急忙忙吃完午饭,坐上了电车。 现在,电车正行驶在原野上。窗外,水田、旱地连成一片。汽车在公路上奔驰。 这时,电车正行驶在大桥上。下面河水在流动。河水很清澈,可以清澈地看见河底。可以看见鱼在游动。远处,一个小孩在挥手。他身旁,牛、马在吃草。 到了爷爷居住的村子。爷爷和奶奶来到门口等着我。爷爷的房子是旧房子,但是很大。登上二楼,大海就在眼前。海岸上,很多人正在全力拉缆绳。渐渐地可以看见网了。网里有很多鱼。和城市不同,乡下的大自然真是很美。 第13课 暑假 大概没有什么比暑假更令学生感到高兴的了。大学在7月初,其他学校在二十四日左右进入暑假。暑假大约1个半月。 很多人利用这个假期去海边、山上,或者去旅行。学生中,也有人去打工。学生由于路费等只要半价,所以在学期间去各地旅行。因此,临近暑假时,去北海道的列车上就挤满了这样的人。从炎热的地方逃避到凉爽的地方去,这是很自然的事。一般在1月、最迟在2月底之前就要预定旅馆。不然的话可能会没有地方住。 暑假里,山上、海边、湖里、河里会出现死人的事,这种事故都是由于不注意引起的。大概只能每个人自己多加注意了。 在东京附近,镰仓等地的海面不起浪,因此挤满了游泳的人。也有人家只在夏季把海边的房子租下来。 暑假里,学校的老师给学生布置作业,但是有的学生叫哥哥或姐姐帮忙。 第14课 各式各样的学生 我就读的大学都有各种各样的学生入学。学生有的是中国人,有的是美国人,有的是英国人。既有年轻的,也有不年轻的。有胖的学生,也有瘦的学生。学生大多边工作边学习。因此,大家看上去都很忙。经常有人边听课边打盹。 我为了学习日本先进的科学技术和日本文化来到日本。预定在这所大学学习3年。既然特意来了日本,所以每天都很努力学习。即便如此,考试之前还是很紧张。其他学生也是这

新视野大学英语5课文翻译(全)

教育界的科技革命 如果让生活在年的人来到我们这个时代,他会辨认出我们当前课堂里发生的许多事情——那盛行的讲座、对操练的强调、从基础读本到每周的拼写测试在内的教学材料和教学活动。可能除了教堂以外,很少有机构像主管下一代正规教育的学校那样缺乏变化了。 让我们把上述一贯性与校园外孩子们的经历作一番比较吧。在现代社会,孩子们有机会接触广泛的媒体,而在早些年代这些媒体简直就是奇迹。来自过去的参观者一眼就能辨认出现在的课堂,但很难适应现今一个岁孩子的校外世界。 学校——如果不是一般意义上的教育界——天生是保守的机构。我会在很大程度上为这种保守的趋势辩护。但变化在我们的世界中是如此迅速而明确,学校不可能维持现状或仅仅做一些表面的改善而生存下去。的确,如果学校不迅速、彻底地变革,就有可能被其他较灵活的机构取代。 计算机的变革力 当今时代最重要的科技事件要数计算机的崛起。计算机已渗透到我们生活的诸多方面,从交通、电讯到娱乐等等。许多学校当然不能漠视这种趋势,于是也配备了计算机和网络。在某种程度上,这些科技辅助设施已被吸纳到校园生活中,尽管他们往往只是用一种更方便、更有效的模式教授旧课程。 然而,未来将以计算机为基础组织教学。计算机将在一定程度上允许针对个人的授课,这种授课形式以往只向有钱人提供。所有的学生都会得到符合自身需要的、适合自己学习方法和进度的课程设置,以及对先前所学材料、课程的成绩记录。 毫不夸张地说,计算机科技可将世界上所有的信息置于人们的指尖。这既是幸事又是灾难。我们再也无须花费很长时间查找某个出处或某个人——现在,信息的传递是瞬时的。不久,我们甚至无须键入指令,只需大声提出问题,计算机就会打印或说出答案,这样,人们就可实现即时的"文化脱盲"。 美中不足的是,因特网没有质量控制手段;"任何人都可以拨弄"。信息和虚假信息往往混杂在一起,现在还没有将网上十分普遍的被歪曲的事实和一派胡言与真实含义区分开来的可靠手段。要识别出真的、美的、好的信息,并挑出其中那些值得知晓的, 这对人们构成巨大的挑战。 对此也许有人会说,这个世界一直充斥着错误的信息。的确如此,但以前教育当局至少能选择他们中意的课本。而今天的形势则是每个人都拥有瞬时可得的数以百万计的信息源,这种情况是史无前例的。 教育的客户化 与以往的趋势不同,从授权机构获取证书可能会变得不再重要。每个人都能在模拟的环境中自学并展示个人才能。如果一个人能像早些时候那样"读法律",然后通过计算机模拟的实践考试展现自己的全部法律技能,为什么还要花万美元去上法学院呢?用类似的方法学开飞机或学做外科手术不同样可行吗? 在过去,大部分教育基本是职业性的:目的是确保个人在其年富力强的整个成人阶段能可靠地从事某项工作。现在,这种设想有了缺陷。很少有人会一生只从事一种职业;许多人都会频繁地从一个职位、公司或经济部门跳到另一个。 在经济中,这些新的、迅速变换的角色的激增使教育变得大为复杂。大部分老成持重的教师和家长对帮助青年一代应对这个会经常变换工作的世界缺乏经验。由于没有先例,青少年们只有自己为快速变化的"事业之路"和生活状况作准备。

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