| 研究生: |
曾保仁 Tseng, Pao-Jen |
|---|---|
| 論文名稱: |
微槽內緩燃焰轉爆震焰機制之數值解析 Numerical Analysis on the Mechanisms of DDT in Micro Channels |
| 指導教授: |
吳明勳
Wu, Ming-Hsun |
| 學位類別: |
碩士 Master |
| 系所名稱: |
工學院 - 機械工程學系 Department of Mechanical Engineering |
| 論文出版年: | 2013 |
| 畢業學年度: | 101 |
| 語文別: | 中文 |
| 論文頁數: | 108 |
| 中文關鍵詞: | 緩燃焰轉爆震焰機制 、微爆震 |
| 外文關鍵詞: | Deflagration-to-detonation transition, microdetonation |
| 相關次數: | 點閱:51 下載:2 |
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本研究藉由三維數值模擬一截面為1 mm × 1 mm、長為100 mm、由中心點火往兩端開口傳遞之方槽內反應波與震波生成及傳遞動態,槽內初始為298K靜止之C2H4+3O2,分別針對槽內初始壓力、二氧化碳稀釋與壁面鋸齒三種參數,探討震波與反應波間之交互作用對於緩燃焰加速與轉爆震焰加速過程之影響。
槽內初始壓力會影響燃氣質量燃燒率與分子間碰撞機率,於0.05 MPa下會熄焰且無法向前傳遞;0.1 MPa結果顯示,前導震波的生成不僅預壓縮更預熱了火焰面前方未燃氣體,且完全發展之後的正向回饋效應會使爆震焰產生;0.2 MPa時,由於壓力增加導致質燃燒率與分子間碰撞機率大幅增加,使得反應波尖端速度快速提升,於50 s便成功轉變為爆震焰,DDT所需時間與距離大幅縮短了150 s 與32 mm。等溫壁面373 K、二氧化碳稀釋=0.1條件下,前導震波發展階段中反應波尖端壓力會逐漸消散,使得阻滯效應影響大幅降低,因此無法成功產生爆震焰並熄焰。絕熱壁面、二氧化碳稀釋=0與=0.1兩組案例中,二氧化碳稀釋會使得化學反應速率變慢,導致DDT所需時間與距離增加了59 s與12.3 mm。
壁面鋸齒案例中,於一點火後便迅速引燃,並產生前導震波於反應波前方,震波接觸鋸齒之後反射至中心會進一步累積反應波壓力使DDT產生;由反應波速度圖可以得知,壁面加入鋸齒壁面鋸齒能使原本無法產生DDT之直槽成功由緩燃焰轉變為爆震焰。
Three dimensional numerical simulation was used to model the formation and propagation of shock waves and reaction waves propagated from the middle end toward to open end in a millimeter-size channel, which was 1 mm depth and 100 mm length. Initial conditions for channel were C2H4+3O2 at 298 K. The effects of interaction between two waves on deflagration acceleration and deflagration-to-detonation transition (DDT) were observed for different initial channel pressure, CO2 dilution and zigzag cases.
The initial pressure would affect mixture burning rate and probability of molecular collision. As a result, reaction wave could not propagated and quenched in 0.05 MPa case. In 0.1 MPa case, the results showed that the shock wave not only pre-compression but also pre-heat the unburned gas in front of reaction wave. Detonation occurred due to positive feedback effect flame accelerated and DDT transition occurred. In 0.2 MPa, burning rate and probability of molecular collision increased due to large pressure. Velocity of reaction wave increased suddenly and DDT occurred at 50 s. In constant wall temperature 373 K and CO2 dilution =0.1 case, the reaction wave pressure dissipated continuously at leading shock formation stage. The effects of choking decreased results in flame quenching. In adiabatic wall and CO2 dilution =0.1、=0 cases, CO2 dilution would slow the chemical reaction.
In zigzag cases, the flame propagated just after ignited and leading shock formed. Shock wave reflected to the channel centre would accumulate pressure of reaction front and make DDT occur. From figure of reaction wave speed, Sidewall zigzag did make DDT occur in channel that couldn't have DDT at all.
[1]Kagan, L., and Sivashinsky, G. (2003), The transition from deflagration to detonation in thin channels, Combustion and Flame 134, 389-397.
[2]Bychkov, V., Petchenko, A., Akkerman, V., and Eriksson, L.-E. (2005), Theory and modeling of accelerating flame in tubes, Physical Review E 72, 046307 1-10.
[3]Bychkov, V., Akkerman, V., Fru, G., Petchenko, A., and Eriksson, L.-E. (2007), Flame acceleration in the early stage of burning in tubes, Combustion and Flame 150, 263-276.
[4]Kagan, L. (2007), On the transition from deflagration to detonation in narrow channels, Math. Model. Nat. Phenom. 2(2), 40-55.
[5]Kagan, L., and Sivashinsky, G. (2008), Autoignition due to hydraulic resistance and deflagration-to-detonation transision, Combustion and Flame 154, 186-190.
[6]Kagan, L., and Sivashinsky, G. (2010), On the transition from deflagration to detonation in narrow tubes, Flow Turbulence and Combustion 84, 423-437.
[7]Valiev, D., Bychkov, V., Akkerman, V., Law, C.K., and Eriksson, L.-E. (2010), Flame acceleration in chanels with obstacles in the deflagration-to-detonation transition, Combustion and Flame 157, 1012-1021.
[8]Laderman, A.J., Urtiew, P.A., and Oppenheim, A.K. (1963), On the generation of a shock wave by flame in an explosive gas, Symposium (International) on Combustion 9(1), 265-274.
[9]王俊凱, 預混焰於微管槽內加速機制之研究, 國立成功大學機械工程學系碩士論文, 2010.
[10]邱柏淵, 微槽內爆震焰產生過程中震波與反應波之交互作用, 國立成功大學機械工程學系碩士論文, 2012.
[11]Ott, J.D., Oran, E.S., and Anderson, J.D. (2003), A mechanism for flame acceleration in narrow tubes, AIAA Journal 41(7), 1391-1396.
[12]Gamezo, V.N., and Oran, E.S. (2006), Flame acceleration in narrow channels: Applications for micropropulsion in low-gravity environments, AIAA Journal 44(2), 329-336.
[13]Poludnenko, A.Y., Gardiner, T.A., and Oran, E.S. (2011), Spontaneous transition of turbulent flames to detonations in unconfined media, Physical Review Letters 107(5), 054501.
[14]Wu, M.-H. and Kuo, W.-C. (2013), Accelerative expansion and DDT of stoichiometric ethylene/oxygen flame rings in micro-gaps, Proceedings of the Combustion Institue 34, 2017-2024.
[15]Wu, M.-H., and Kuo, W.-C. (2012), Transition to detonation of an expanding flame ring in a sub-millimeter gap, Combustion and Flame 159, 1366-1368.
[16]Frolov, S.M. (2009), Detonation initiation techniques for pulse detonation propulsion, Progress in Propulsion Physics 1, 321-340.
[17]Frolov, S.M., Semenov, I.V., Komissarov, P.V., Utkin, P.S., and Markov, V.V. (2007), Reduction of deflagration to detonation transition distance and time in a tube with regular shaped obstacles, Physical Chemistry 415(2), 209-213.
[18]Urtiew, P.A., and Oppenheim, A.K. (1966), Experimental observations of transition to detonation in an explosive gas, Proceedings of the Royal Society of London Series a-Mathematical and Physical Sciences 295, 13-28.
[19]Kuznetsov, M., Alekseev, V., Matsukov, I., and Dorofeev, S. (2005), DDT in a smmoth tube filled with a hydrogen-oxygen mixture, Shock Waves 14, 205-215.
[20]Kuznetsov, M., Matsukov, I., Alekseev, V., Breitung, W., and Dorofeev, S., Effect of boundary layer on flame acceleration and DDT, Proc. 20th ICDERS, Montreal, Canada, 2005.
[21]Brailovsky, I., and Sivashinsky, G.I. (2000), Hydraulic resistance as a mechanism for deflagration-to-detonation transition, Combustion and Flame 122, 492-499.
[22]Brailovsky, I., Kagan, L., and Sivashinsky, G.I. (2012), Combustion waves in hydraulically resisted systems, Philosophical Transactions of the Royal Society A 370, 625-646.
[23]Valiev, D., Bychkov, V., Akkerman, V., Eriksson, L.-E., and Marklund, M. (2008), Heating of the fuel mixture due to viscous stress ahead of accelerating flames in deflagration-to-detonation transition, Physics Letters A 372(27-28), 4850-4857.
[24]Bychkov, V., and Akkerman, V. (2006), Explosion triggering by an acceleration flame, Physical Review E 73, 066305 1-11.
[25]Liberman, M.A., Kuznetsov, M., Ivanov, A., and Matsukov, I. (2009), Formation of the preheat zone ahead of a propagating flame and the mechanism underlying the deflagration-to-detonation transition, Physics Letter A 373, 501-510.
[26]Valiev, D.M., Bychkov, V., Akkerman, V., and Eriksson, L.-E. (2009), Different stages of flame acceleration from slow burning to chapman-jouguet deflagration, Physical Review E 80, 036317.
[27]Dorofeev, S.B. (2011), Flame acceleration and explosion safety applications, Proceedings of the Combustion Institute 33, 2161-2175.
[28]Wu, M.-H., and Lu, T.-H. (2012), Development of a chemical microthruster based on pulsed detonation, Journal of Micromechanics and Microengineering 22, 105040.
[29]呂宗訓, 脈衝爆震微推進器之概念驗證及原型發展, 國立成功大學機械工程學系碩士論文, 2012.
[30]Bychkov, V., Akkerman, V., Valiev, D., and Law, C.K. (2010), Role of compressibility in moderating flame acceleration in tubes, Physical Review E 81, 026309 1-9.
[31]Bychkov, V., Valiev, D., Akkerman, V., and Law, C.K. (2012), Gas compression moderates flame acceleration in deflagration-to-detonation transition, Combustion Science and Technology 184, 1066-1079.
[32]Valiev, D., Akkerman, V., Kuznetsov, M., and Erikkson, L.-E. (2013), Influence of gas compression on flame acceleration in the early stage of burnign in tubes, Combustion and Flame 160(1), 97-111.
[33]Wu, M.-H., and Kuo, W.-C. (2012), Transmission of near-limit detonation wave through a planar suddent expansion in narrow channel, Combustion and Flame 159, 3414-3422.
[34]郭維鈞, 微槽內爆震焰通過二維突擴之傳遞特性, 國立成功大學機械工程學系碩士論文, 2011.
[35]STAR-CD Methodology v. 4.08, CD-adapco, 2008.
[36]Yakhot, V., and Orszag, S.A. (1986), Renormalization group analysis of turbulence. I. Basic theory, J. Scientfic Computing 1, 1-51.
[37]Yakhot, V., Orszag, S.A., Thangam, S., Gatski, T.B., and Speziale, C.G. (1992), Development of turbulence models for shear flows by a double expansion technique, Physics of Fluids A-Fluid Dynamics 4(7), 1510-1520.
[38]Rodi, W., Influence of buoyancy and rotation on equations for the turbulent length scale, in Proc. 2nd Symp. on Turbulent Shear Flows, London, England, 1979.
[39]Baurle, R.A., and Eklund, D.R. (2002), Analysis of dual-mode hydrocarbon scramjet operation at mach 4-6.5, Journal of Propulsion and Power 18(5), 990-1002.
[40]Issa, R.I. (1986), Solution of the implicitly discretized fluid-flow equations by operator-splitting, Journal of Computational Physics 62(1), 40-65.
[41]Issa, R.I., Ahmadibefrui, B., Beshay, K.R., and Gosman, A.D. (1991), Solution of the implicitly discretized reacting flow equations by operator-splitting, Journal of Computational Physics 93(2), 388-410.
[42]Lai, K.Y.M., Numerical analysis of fluid transport phenomena, Ph.D Thesis, Unisversity of London, 1983.
[43]Leschziner, M.A. (1980), Practical evaluation of three finite difference schemes for the computation of steady-state recirculating flows, Computer Methods in Applied Mechanics and Engineering 23(3), 293-312.