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英語文章總結(jié)
英語論文總結(jié)怎么寫【1】
英語論文寫作論文結(jié)論部分(Conclusion)寫作特點(diǎn)總結(jié)Conclusion Conclusion 是作者對(duì)所研究課題進(jìn)行的總體性討論，具有嚴(yán)密的科學(xué)性和客觀性，反映 本研究課題的價(jià)值，同時(shí)對(duì)以后的研究具有指導(dǎo)意義。
Conclusion 與 Introduction 遙相呼應(yīng)，因?yàn)?Introduction 部分介紹了本課題的研究目的， 那么 Conclusion 要告訴讀者這些目的是否達(dá)到，在研究中做了哪些工作，取得了什么結(jié)果， 這些結(jié)果說明了什么問題，有何價(jià)值和意義，研究過程中存在或發(fā)現(xiàn)了哪些問題，原因是什 么，建議如何解決等。
Conclusion 的具體內(nèi)容通常包含以下幾個(gè)部分
(1) 概括說明本課題的研究內(nèi)容、結(jié)果及其意義與價(jià)值。
(2) 比較具體地說明本研究證明了什么假設(shè)或理論，得出了什么結(jié)論，研究結(jié)果有何實(shí) 用價(jià)值，有何創(chuàng)造性成果或見解，解決了什么實(shí)際問題，有何應(yīng)用前景等。
(3) 與他人的相關(guān)研究進(jìn)行比較。
(4) 本課題的局限性、不足之處，還有哪些尚待解決的問題。
(5)展望前景，或指出進(jìn)一步研究的方向。
Conclusion 通常使用現(xiàn)在時(shí)態(tài)Result 和 Conclusion 本次選取 5 篇文章， 第一篇，論文中的主要 Result 已在第 2 部分和第三部分中敘述，在 Conclusion 又重新總 結(jié)了一下。
第二篇，論文中的主要 Result 寫在 Conclusion 中。
第三篇，論文中的主要 Result 寫在第 3 部分(3.CASE STUDIES AND RESULTS)中， Result 和 Conclusion 是分開的。
第四篇，論文中的主要 Result 已第 4 部分的(IV.
Results and Discussion)中進(jìn)行敘述， Result 和 Conclusion 是分開的。
第五篇， 論文中的主要 Result 已第 4 部分的 Results and discussion) (4.
中進(jìn)行敘述，Result 和 Conclusion 是分開的。第1篇 題目：An overview of NACA 6-digit airfoil series characteristics with reference to airfoils for large wind turbine bladesIV.
ConclusionsThe two-dimensional aerodynamics characteristics of the NACA 63 and 64 six-digit series of airfoils measured in the NASA LTPT have been investigated, with a view to verify RFOIL calculations at high Reynolds numbers.
The following conclusions can be drawn
- The zero-lift angle of the NACA 64-618 airfoil needs to be adjusted with -0.4 degrees.
- The zero-lift angle of The NACA 63-615 needs to be corrected with -0.87 degrees in the smooth case and with +1 degree in case of wrap around roughness.
-The maximum lift coefficients predicted with RFOIL match the LTPT data well at Re=3x106, but under predict the Cl,max at Re=6x106 by 3.5 % , up to 6.5% at Re=9x106.
-It is uncertain if the established differences in lift between experiment and calculations are caused by a constant bias in the measurements or by the fact that the RFOIL code fails to predict the right level of maximum lift.
-RFOIL consistently under predicts the drag coefficient.
The difference is about 9% for a wide range of airfoils and Reynolds numbers -NACA standard roughness causes a reduction in the lift coefficient of 18% to 20% for most airfoils from the NACA 64 series -The zero-lift angle of airfoil NACA 64-418 with wrap-around roughness needs a correction of +0.54 degrees.
-Wind tunnel experiments and side-by-side tests in the field with one clean rotor need to be done to be able to better predict the effects of roughness.
寫作特點(diǎn)
內(nèi)容：第 1 句，概括了文章的的主要研究內(nèi)容。第 2 句至第 8 句逐條的列出了文章的得出結(jié) 論。
使用了被動(dòng)語態(tài)，The two-dimensional aerodynamics characteristics of the NACA 63 and 64 six-digit series of airfoils measured in the NASA LTPT have been investigated have been investigated.
主要時(shí)態(tài)為一般現(xiàn)在時(shí)態(tài)第2篇題目
HIGH-LIFT ENHANCEMENT USING ACTIVE FLOW CONTROLV.
CONCLUSIONS The high-lift performance of an airfoil with a single-element flap is enhanced significantly using an active flow control system consisting of spanwise fluidic actuators that are integrated near the separation point.
Spanwise arrays of spanwise-oscillating or non-oscillating jets issue tangentially to the local surface from a miniature downstreamfacing surface step.
Jet actuation leads to flow attachment of varying streamwise extent that depends on the jet momentum coefficient and the formation of a low pressure domain near the juncture between the main body and the flap.
As a result, lift is increased substantially, by as much as ? CL = 1.40, 1.22 and 1.04 at Rec = 6.7?105, 8.3?105 and 1.0?106, respectively, for α = 4?.
In the present experiments, three spanwise rows of fluidic jets are placed in the vicinity of the juncture and operated in various combinations leading to significant increases in lift.
The upstream (x/c = 0.59) and middle (x/c = 0.61) actuators, which are closest to separation (x/c = 0.62) are most effective, while the downstream actuator (x/c = 0.64) only produces a significant lift increment when operated in conjunction with one of the other actuators.
The degree of flow attachment increases with jet momentum coefficient and simultaneous operation of multiple actuators can increase the lift increment further even when the flow is attached.
Actuation results in a strong suction peak near the juncture (Cp ~ ?7.5) and also leads to increases in suction on the main body of the airfoil and near the leading edge.
The lift increment is measured over a range of angles of attack (0? < α < 12?) and is accompanied by an increase in lift-induced pressure drag and an increase in nose-down pitching moment.
It is shown that the high-lift performance can be improved significantly by design modifications of the surface interface between the jet actuators and the surrounding flow.
In particular, modifying the jet orifices from a “stepped” to a “recessed” configuration enhances the interaction of the jets with the cross flow, resulting in increased lift for a given momentum coefficient, particularly at lower levels of C? .
The recessed design also reduces the loss in lift caused by the presence of the orifices and the attached flow exhibits significantly stronger suction peaks near the flap juncture and the leading edge.
At C? = 0.36% the upstream actuator yields ? CL = 0.
and 0.79 for the stepped and recessed 57 configurations, respectively, and operating the combination of upstream and middle actuators at C? = 0.36% each yields ? CL = 0.78 and 0.92, respectively.
The effect of the actuator jets on the attached flow is characterized using PIV measurements of the flow field over the flap and additional high-magnification measurements in the vicinity of the actuators.
In the absence of actuation, the flow separates near the juncture between the flap and the main body (x/c = 0.62), forming a recirculating domain over the flap and a detached vorticity layer.
Actuation leads to complete flow attachment through the trailing edge with significant acceleration of the flow within the attached boundary layer downstream of the actuators and outside of the boundary layer along most of the flap.
At C= 1.6% an interaction domain containing a cross-stream velocity peak (~2.3 times the maximum speed of the jet under quiescent conditions) is formed along the flap between the actuator jet and the free stream flow that is particularly apparent using the recessed configuration.這篇文章的結(jié)論部分很特殊，統(tǒng)計(jì)的結(jié)果為 565 個(gè)單詞，包含了 4 個(gè)段落。
第 1 段概括了文章的主要研究內(nèi)容(active flow control system)，第 2 段到第 4 段主要說明了文 章的研究方法(experiment，PIV)，以及一些具體的結(jié)果。主要時(shí)態(tài)為一般現(xiàn)在時(shí)態(tài)第3篇題目
REPRESENTATION METHOD EFFECTS ON GENETIC ALGORITHM IN 2-DAIRFOIL DESIGNVIBRATIONAL4.
CONCLUSION In this article, Bezier and Parsec representation methods are tested in two different flow conditions; subsonic and transonic flows.
In the fist test case both representation methods are compared via VGA optimization tool under the subsonic flow conditions.
The comparison between Bezier and Parsec representation methods is shown in Fig.
8.
This plot emphasizes the superiority of Parsec representation method.
In the second test case both representation methods are compared via VGA optimization tool under the transonic flow conditions.
The comparison between Bezier and Parsec representation methods is shown in Fig.
11.
This plot emphasizes the superiority of Bezier representation method.
From these cases it is concluded that Parsec method is more global and more efficient than Bezier method in subsonic flows.
However, Bezier method is more flexible than Parsec method within transonic flows.本篇文章相比于上篇文章內(nèi)容上比較簡短：統(tǒng)計(jì)結(jié)果為 134 個(gè)單詞，包含 1 個(gè)段落 第 1 句，概括了文章的的主要研究內(nèi)容。第 2 句至第 7 句回顧了文章中的兩個(gè)算例。第 8 句說明了本文方法的優(yōu)越性，最后一句說明了本文方法的不足。
主要時(shí)態(tài)為一般現(xiàn)在時(shí)態(tài)句型
In this article, The comparison between is shown in Fig.
8.
From these cases it is concluded that However,第4篇 題目
Unsteady Flow Simulation of a High-Lift configuration using a Lattice Boltzmann ApproachV.
Conclusions Simulations of a generic high-lift geometry were carried out using the Lattice Boltzmann based code PowerFLOW with the framework of the 1st AIAA CFD High Lift Prediction Workshop held in 2010.
The results shown here were the only unsteady simulations among all workshop participants and show excellent agreement of drag and lift forces as well as cp distributions for all workshop cases.
Good predictions in the region of maximum lift were a particularly distinguishing feature of the Lattice Boltzmann simulations, indicating the importance of unsteady simulations in correctly capturing strongly separated flow structures.
The slight over-prediction of cL,max observed for the baseline case was shown to be largely attributable to the absence of slat and flap brackets in the simulations.
Adding these brackets (Case 3 of the workshop) shows a significant reduction of lift in particular at the higher angle of attack, bringing the simulation results to almost perfect agreement with measured results.
The effect of changing flap angles was also well captured by the simulations.
The position of laminar-to-turbulence transition was set for most of the simulations presented here based on published experimental results since the method used for the current study uses a wall model rather than fully resolving the boundary layer.
Fully turbulent simulations were carried out for selected configurations and showed a significant reduction of lift.
In addition to the workshop cases a study of wind tunnel blockage effects is shown here.
Adding walls in the simulation corresponding to the dimensions of the wind tunnel led to a change of predicted forces consistent with the corrections applied to the experimental results.
Computational times required for the unsteady simulations were generally in the same order of magnitude or even slightly below as the RANS simulations presented by other workshop participants, confirming the high level of efficiency of the unsteady Lattice Boltzmann method.
Overall, this method was shown to be an interesting and viable alternative to the predominantly used RANS methods for the simulation of high-lift wings.本篇文章的結(jié)論也相對(duì)較長,統(tǒng)計(jì)結(jié)果為 329 個(gè)單詞，包含 4 個(gè)段落 第 1 段概括了文章的的主要研究內(nèi)容。
第 2 段對(duì)文章中的使用的計(jì)算方法中的 laminar-to-turbulence transition 進(jìn)行了說明。
第 3 段文章中的使用的計(jì)算方法中的一點(diǎn)(Adding walls in the simulation)進(jìn)行了說明。
第 4 段對(duì)文章的計(jì)算效率進(jìn)行了說明。進(jìn)一步說明文章方法的優(yōu)越性。主要時(shí)態(tài)為一般現(xiàn)在時(shí)態(tài)第5篇 題目
Design of a new urban wind turbine airfoil using a pressure-load inverse method 5.
Conclusions A pressure-load inverse design method was successfully applied to the design of a high-loaded airfoil for application in a small wind turbine for urban environment.
The pressure distribution of the designed blade section shows a smooth increase of the blade pressure-load, defined as the pressure difference between the upper and the lower sides of the section, from the leading edge up to 20% of the axial chord.
From 20% up to 80% of the axial chord, the pressure-load is almost constant and it reduces smoothly toward the trailing edge.
The experimental testing of the new blade section, as an isolated airfoil, confirmed the high maximum lift and a moderate drag.
Future developments will consider the application of the current design method with an optimization of the thickness distribution for viscous flow.
Due to the specification of the blade load, this methodology will reduce the drag without changing the lift.
本篇文章的結(jié)論相對(duì)比較簡潔,統(tǒng)計(jì)結(jié)果為 149 個(gè)單詞，包含 1 個(gè)段落 第 1 句概括了文章的的主要研究內(nèi)容。
第 2 句至第 4 句對(duì)文章方法進(jìn)行了再次說明 第 5 句進(jìn)行了展望 第 6 句提到本文方法的優(yōu)越性。
高考作文的結(jié)尾手法【2】
結(jié)尾是文章留給閱卷老師的最終印象，即結(jié)論性印象。因此，一個(gè)好的結(jié)尾應(yīng)該是能打動(dòng)閱卷老師的內(nèi)心，
激起他們的共鳴，從而對(duì)文章做出最好的也是最終的評(píng)價(jià)。
結(jié)尾要緊扣段落主題，又要有所拓展。結(jié)尾要求簡潔有力，意味雋永。好的結(jié)尾能使全文增色。結(jié)尾句寫作看似很難，但有很多方法可以借鑒。下面就結(jié)合實(shí)例給大家介紹一下英語作文結(jié)尾的具
體方法：
書面表達(dá)結(jié)尾“七法”(一)總結(jié)性結(jié)尾
總結(jié)性結(jié)尾常用于任務(wù)或活動(dòng)介紹結(jié)束后吧對(duì)文章進(jìn)行總結(jié)，這一總結(jié)對(duì)原文既是一種回顧，又是一種概
括，有時(shí)候與文章開頭形成呼應(yīng)，從而有效增強(qiáng)文章的連貫性、邏輯性和可讀性。起到點(diǎn)明主題，深化主題，畫龍點(diǎn)睛的效果。
例1：Inshort,thestudentshavenotarrivedatanyagreementyet.(2004湖北)
解析：2004年湖北試題是關(guān)于英語學(xué)習(xí)的討論，結(jié)尾用一句話交待了雙方的爭論結(jié)果，顯得簡潔有力。例2：AsfarasIknow,everyoneishappyaboutthisnewarrangementofthings.(NMET2001)
解析：2001年高考英語書面表達(dá)主題是關(guān)于減輕學(xué)生學(xué)習(xí)負(fù)擔(dān)。這一總結(jié)性結(jié)尾與文首的Inshort,things
havebeguntoimprovesinceschoolswerecalledontoreducelearningload.形成照應(yīng)，它也是對(duì)全文的一種概括與總結(jié)，體現(xiàn)了減負(fù)后作者興奮的心情。
(二)引用性結(jié)尾
引用名人名言結(jié)尾，是使文章大放異彩的好方法。
例：Thestorytellsusthatifyouwanttogetsomething,youmustworkhardforit.Remember,nopains,nogains!(2005廣東)
解析：2005年廣東試題要求寫出故事《守株待兔》。范文引用了名言“Nopains,nogains.”體現(xiàn)了作者良好
的英語功底，同時(shí)也給人留下了深刻的印象。
(三)反問式結(jié)尾
反問也是體現(xiàn)文章力度的一個(gè)好方法。用反問結(jié)尾雖然形式是問句，但意義多是肯定的，具有強(qiáng)調(diào)作用，
能引起讀者深思。
例1：Therefore,Ithinkit’sagoodideaforyoutoreturn.Sowhatareyouwaitingfor?(2005湖北)
解析：2005年湖北試題盡管是應(yīng)用文，但范文以“Sowhatareyouwaitingfor?”的反問形式為文章做出了鼓
動(dòng)性的結(jié)尾，給人以躍躍欲試的感覺，無疑會(huì)增加評(píng)卷者對(duì)文章的影響分。例2：Everyoneshouldlearntodohousework.Don'tyouagree,boysandgirls?
解析：這是以“Shouldwelearntodohousework?”為題的一篇文章的結(jié)尾。顯然，作者要表達(dá)的觀點(diǎn)是每
個(gè)人都應(yīng)該dohousework,作者通過結(jié)尾的反問句強(qiáng)調(diào)了文章的主題，增強(qiáng)了文章的形式和效果。
(四)激勵(lì)性結(jié)尾
結(jié)尾表示對(duì)將來的展望，或期待讀者投入某種行動(dòng)，或者對(duì)活動(dòng)發(fā)出號(hào)召和鼓勵(lì)性的口號(hào)。例：Dearfellowstudents,let’sstartfightnowandsparenoefforttodoalittlebiteveryday,everyhour,and
everyminute!(2005江蘇)
解析：2005年江蘇卷書面表達(dá)的主題是建設(shè)和諧社會(huì)。這篇文章的結(jié)尾號(hào)召所有學(xué)生行動(dòng)起來，為建設(shè)和
諧社會(huì)盡自己的一份力，通過“everyday,everyhour,andeveryminute”升華了主題，增強(qiáng)了文章的感召(五)祝愿性結(jié)尾
祝愿性結(jié)尾常用于活動(dòng)介紹、未來展望、各種信件、便條等文體的末尾對(duì)主人公參加特定的活動(dòng)給予衷心
祝愿。這種結(jié)尾感情真摯，極易打動(dòng)閱卷老師。例1：IamsurewewillbothgainabetterunderstandingoftheelderlyinChina.Ifyouhaveanysuggestions,pleaseletusknow.(2007湖北)
解析：2007年湖北卷書面表達(dá)主題是和國際學(xué)校的學(xué)生一起去敬老院慰問老人。這一祝愿性結(jié)尾表達(dá)了通
過這次活動(dòng)同學(xué)們一定能增加對(duì)中國老人的生活了解。誠摯的祝愿體現(xiàn)了和國際學(xué)生間的友誼，并征求對(duì)方意見，讀來真實(shí)生動(dòng)。
例2：Inaddition,Ineedtogetalongwellwithmyclassmatesandteachersatcollege.IthinkIwillhavea
wonderfulcollegelife.(2007遼寧)
解析：祝愿式的結(jié)尾，體現(xiàn)出作者對(duì)未來大學(xué)生活的向往和自信之情，令人印象深刻。(六)結(jié)論式結(jié)尾
這種結(jié)尾常用于各種活動(dòng)介紹及故事敘述中交代活動(dòng)及故事的結(jié)局，雖不驚天動(dòng)地、波瀾壯闊。卻也自然
真實(shí)，順理成章。
例：WangHongbecameournewmontior.Thewholeclasscheeredforher,andshepromisedtodothebestshe
couldforusall.(2007北京)
解析：2007年北京卷的開放性作文主題是競選班長。作者在結(jié)尾介紹了競選的最后結(jié)果，字里行間流露出
對(duì)新班長的信任和期待。至此，文章自然而然地結(jié)束。這樣平穩(wěn)自然的結(jié)尾也不失為一種好的選擇。
(七)含蓄性結(jié)尾
用比喻或含蓄的手法不直接點(diǎn)明作者的看法，而是讓讀者自己去領(lǐng)會(huì)和思考。例：Thebirdwassetfree.Seeingthebirdflyinghappilyinthesky,bothLiMingandhisgrandpasmiled.(2006遼
寧)
解析:2006年遼寧卷書面表達(dá)的內(nèi)容是李明和爺爺一起放飛小鳥的故事。作者通過對(duì)“將小鳥放飛”的場景
的描寫：“flyinghappily,smiled”,含蓄地交待了主人公的態(tài)度和看法，結(jié)尾起到畫龍點(diǎn)睛的作用，而且顯得意味深長，以情感人。
文章的結(jié)尾沒有一成不變的模式，我們可以根據(jù)表達(dá)主題的需要靈活創(chuàng)造。一般的習(xí)慣是：
記敘文和描寫文經(jīng)常采用自然結(jié)尾的方法;
說理性和邏輯性較強(qiáng)的說明文和議論文則往往都有結(jié)束語，以便使文章首尾呼應(yīng)，結(jié)構(gòu)完整。
常用結(jié)尾句
Ingeneral/aboveall/Withtheresultthat/Asaresult/consequently…AsfarasIamconcerned/Asforme,…
Inmypointofview,Ilike/preferAmuchmorethanB.
IstillpreferA,however,fortheyteachmenotonlytobe…butalsotobe…Thereisnodoubtthat…
Inordertomakeourworldabetterplacetolivein,weshouldmakeeffortsto…Toalargeextent…
Ifallabovementionedmeasuresareachieved,…Whereveryouare,youwillfindpeople….
Soclear/obviousitisthattherearequitedifferentopinionsonit.
Fromwhathasbeendiscussedabove,wemaysafelydrawtheconclusionthat…Insummary/Inshort,itiswiser…
Tosumup/Onthewhole/Inbrief/Inaword,itistruethatweshouldbringaboutbothpositiveandnegative
results.Butwecantryoutbesttoreducethenegativeinfluencetotheleastextent.Obviously,wecandrawtheconclusionthat…
Thus,itcanbeconcludedthat…/Therefore,wecanfindthat…
開頭與結(jié)尾的三項(xiàng)基本原則1.用好原句，不另辟蹊徑高考書面表達(dá)題往往會(huì)給出開篇句或結(jié)尾句，我們只需要用好這些已給信息即可。因?yàn)檫@些句子既
給我們提供了信息，又從一定程度上規(guī)定了我們寫作的文體。2.用好原句，不另辟蹊徑
高考書面表達(dá)題往往會(huì)給出開篇句或結(jié)尾句，我們只需要用好這些已給信息即可。因?yàn)檫@些句子既
給我們提供了信息，又從一定程度上規(guī)定了我們寫作的文體。3.恰到好處，不狗尾續(xù)貂
和開頭一樣，好的尾句也可以反映出作者總攬全文的能力，同時(shí)，它也應(yīng)該是控制字?jǐn)?shù)、畫龍點(diǎn)睛之筆。
好的尾句應(yīng)該照應(yīng)全文，總結(jié)全篇，干凈利落，使全文結(jié)構(gòu)緊湊。
文章結(jié)尾的作用是概括全文內(nèi)容，進(jìn)一步強(qiáng)調(diào)或肯定文章的中心思想，使文章意義表達(dá)得更加深刻。文章結(jié)尾的形式也是多種多樣的，常見的有以下幾種：
1.首尾呼應(yīng)，畫龍點(diǎn)睛在文章的結(jié)尾，把含義較深的話放在末尾，以點(diǎn)明主題，深化主題，起到畫龍點(diǎn)睛的效果。如"ICannotForgetHer"(我忘不了她)的結(jié)尾：
Afterherdeath,Ifeltasifsomethingweremissinginmylife.Iwassadoverherpassingaway,butIknewshewouldnothavehadanyregretsathavinggivenherlifeforthebenefitofthepeople.
2.重復(fù)主題句結(jié)尾回到文章開頭闡明的中心思想或主題句上，達(dá)到強(qiáng)調(diào)的效果。如“ILoveMyHomeTown”(我愛家鄉(xiāng))的結(jié)尾：
Ilovemyhometown,andIloveitspeople.Theytoohavechanged.Theyaregoingallouttodomoreforthegoodofourmotherland.
3.自然結(jié)尾隨著文章的結(jié)束，文章自然而然地結(jié)尾。如“Fishing”(釣魚)的結(jié)尾：
Icaughtasmanyastwentyfishintwohours,butmybrothercaughtmanymore.Tiredfromfishing,welaydownontheriverbank,bathinginthesun.Wereturnedhomeverylate.4.含蓄性的結(jié)尾
用比喻或含蓄的手法不直接點(diǎn)明作者的看法，而是讓讀者自己去領(lǐng)會(huì)和思考。如“ADayofHarvesting”(收割的日子)的結(jié)尾：
Eveningcamebeforewerealizedit.Weputdownoursicklesandlookedateachother.Ourclotheswerewetwithsweat,butoneveryfacetherewasasmile.5.用反問結(jié)尾
雖然形式是問句，但意義卻是肯定的，并具有特別的強(qiáng)調(diào)作用，引起讀者深思。如"ShouldWeLearntoDoHousework?"(我們要不要學(xué)做家務(wù)?)的結(jié)尾。
Everyoneshouldlearntodohousework.Don’tyouagree,boysandgirls?
6.指明方向，激勵(lì)讀者結(jié)尾表示對(duì)將來的展望，或期待讀者投入行動(dòng)。如“Let’sGoinforSports”(讓我們參加體育運(yùn)動(dòng))的結(jié)尾：Aswehavesaidabove,sportscanbeofgreatvalue.Theynotonlymakepeoplelivehappilybutalsohelppeopletolearnvirtuesanddotheirworkbettter.Asoundmindisinasoundbody.Let’sgoinforsports.
文章的結(jié)尾沒有一定的模式，可以根據(jù)表達(dá)主題的需要靈活創(chuàng)造。一般的習(xí)慣是，一些記敘文和描寫文經(jīng)常采用自然結(jié)尾的方法;但說理性和邏輯性較強(qiáng)的說明文和議論文則往往都有結(jié)束語，以便使文章首尾呼應(yīng)，結(jié)構(gòu)完整。
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