
董威
教授所在系所:工程熱物理研究所
辦公電話:021-34204410
電子郵件:wdong@sjtu.edu.cn
通訊地址:機(jī)動(dòng)大樓A樓211室
個(gè)人主頁(yè):
教育背景
1996-1999 上海交通大學(xué) 工程熱物理專業(yè) 博士
1994-1996 上海交通大學(xué) 工程熱物理專業(yè) 碩士
1988-1992 北京航空航天大學(xué) 航空動(dòng)力專業(yè) 學(xué)士
工作經(jīng)歷
1992.08 - 1994.08 沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所 助理工程師
1999.04 - 2001.11 上海飛機(jī)研究所 工程師
2001.12 - 2015.12 上海交通大學(xué)機(jī)械與動(dòng)力工程學(xué)院 副教授
2015.12 - 上海交通大學(xué)機(jī)械與動(dòng)力工程學(xué)院 教授、博導(dǎo)
研究方向
1、航空動(dòng)力系統(tǒng)的流動(dòng)傳熱及熱管理
2、航空動(dòng)力系統(tǒng)總體性能及仿真
3、飛機(jī)及航空發(fā)動(dòng)機(jī)結(jié)冰與防冰
4、交叉學(xué)科的流體力學(xué)與傳熱學(xué)
5、航空、航天、新能源等領(lǐng)域的流體及傳熱冷卻技術(shù)
6、高速飛行器氣動(dòng)加熱及熱防護(hù)
學(xué)術(shù)兼職
中國(guó)航空學(xué)會(huì)會(huì)員、中國(guó)宇航學(xué)會(huì)會(huì)員、AIAA Senior Member、ASME Member、中國(guó)能源學(xué)會(huì)會(huì)員
上海航空學(xué)會(huì)空氣動(dòng)力學(xué)專委會(huì)委員、上海航空學(xué)會(huì)航空動(dòng)力專委會(huì)委員
《航空發(fā)動(dòng)機(jī)》編委、《計(jì)算物理》編委、《實(shí)驗(yàn)流體力學(xué)》編委
課程名稱:航空航天動(dòng)力裝置 授課對(duì)象:本科生 學(xué)時(shí):72 學(xué)分:4
課程名稱:推進(jìn)原理 授課對(duì)象:研究生 學(xué)時(shí):36 學(xué)分:2
課程名稱:傳熱學(xué) 授課對(duì)象:本科生 學(xué)時(shí):48 學(xué)分:3
課程名稱:計(jì)算流體力學(xué) 授課對(duì)象:研究生 學(xué)時(shí):36 學(xué)分:2
科研項(xiàng)目
2025-2026 動(dòng)力裝置VFG滑油散熱系統(tǒng)及散熱器性能仿真分析,中國(guó)商用飛機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2024-2025 發(fā)動(dòng)機(jī)混合相和冰晶分析方法開發(fā)技術(shù),中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2023-2025 高精度燃機(jī)性能仿真模型開發(fā),中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2022-2024 基于設(shè)計(jì)與試驗(yàn)協(xié)同的燃?xì)廨啓C(jī)整機(jī)性能仿真建模及評(píng)估預(yù)測(cè)平臺(tái)技術(shù)研究,中國(guó)航發(fā)沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所,項(xiàng)目負(fù)責(zé)人
2022-2024 航空發(fā)動(dòng)機(jī)靜止部件防冰優(yōu)化設(shè)計(jì)方法研究及工具開發(fā),中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2022-2024 非線性邊界條件對(duì)空氣系統(tǒng)性能影響機(jī)理及空氣系統(tǒng)性能仿真建模方法研究,中國(guó)航發(fā)沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所,項(xiàng)目負(fù)責(zé)人
2021-2022 燃?xì)廨啓C(jī)高響應(yīng)過渡態(tài)仿真技術(shù)研究,中國(guó)航發(fā)沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所,項(xiàng)目負(fù)責(zé)人
2021-2022 間冷循環(huán)燃機(jī)性能修正方法研究,中國(guó)航發(fā)沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所,項(xiàng)目負(fù)責(zé)人
2020-2021 緊湊換熱器試驗(yàn)驗(yàn)證技術(shù)研究,中國(guó)航發(fā)沈陽(yáng)航空發(fā)動(dòng)機(jī)設(shè)計(jì)研究所,項(xiàng)目負(fù)責(zé)人
2020-2021 基于試驗(yàn)信息的空氣系統(tǒng)對(duì)部件性能影響因素高精度分析,中國(guó)航發(fā)四川渦輪研究院,項(xiàng)目負(fù)責(zé)人
2019-2021 大溫差高速射流條件下強(qiáng)迫對(duì)流換熱預(yù)測(cè)模型,國(guó)家數(shù)值風(fēng)洞工程項(xiàng)目,項(xiàng)目負(fù)責(zé)人
2018-2020 笛形管防冰系統(tǒng)內(nèi)外流耦合仿真工具和快速優(yōu)化設(shè)計(jì)工具,中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2018-2020 CJ-1000A T25傳感器防冰試驗(yàn),中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2018-2020 對(duì)轉(zhuǎn)槳扇氣動(dòng)設(shè)計(jì)及流動(dòng)特性研究,民機(jī)專項(xiàng), 項(xiàng)目負(fù)責(zé)人
2016-2019 國(guó)家自然科學(xué)基金項(xiàng)目(11572195)渦扇發(fā)動(dòng)機(jī)吸入冰晶的融化凍結(jié)機(jī)理分析及數(shù)值模擬,項(xiàng)目負(fù)責(zé)人
2015-2019 國(guó)家重點(diǎn)基礎(chǔ)研究發(fā)展計(jì)劃(編號(hào):2015CB755800)飛機(jī)結(jié)冰致災(zāi)與防護(hù)關(guān)鍵基礎(chǔ)問題研究---基于結(jié)冰臨界與能量控制的熱防冰理論和方法研究,交大子課題負(fù)責(zé)人
2014-2017 國(guó)家自然科學(xué)基金項(xiàng)目(51376122)沖蝕磨損對(duì)鈦基微-納米結(jié)構(gòu)超疏水表面積冰粘附強(qiáng)度的影響機(jī)理研究,主要參與人
2013-2016 國(guó)家自然科學(xué)基金項(xiàng)目(11272212)大涵道比渦扇發(fā)動(dòng)機(jī)部件表面結(jié)冰粘附特性及冰聚集特性的研究,項(xiàng)目負(fù)責(zé)人
2011-2013 國(guó)家自然科學(xué)基金項(xiàng)目(51076103)進(jìn)氣帽罩結(jié)冰特性與旋轉(zhuǎn)和表面特性的相關(guān)性研究,項(xiàng)目負(fù)責(zé)人
2007-2010 國(guó)家自然科學(xué)基金項(xiàng)目(10772118)導(dǎo)葉初始結(jié)冰狀態(tài)下流型演變、換熱機(jī)理研究,項(xiàng)目負(fù)責(zé)人
2017-2018 結(jié)冰與防冰噴霧系統(tǒng)設(shè)計(jì)開發(fā),中國(guó)航發(fā)四川燃?xì)鉁u輪研究院,項(xiàng)目負(fù)責(zé)人
2017-2018 CJ-1000AXH引氣管路流量特性試驗(yàn),中國(guó)航發(fā)商用航空發(fā)動(dòng)機(jī)有限責(zé)任公司,項(xiàng)目負(fù)責(zé)人
2016-2018 Heat Exchanger Design for Additive Manufacturing,項(xiàng)目負(fù)責(zé)人
2013-2015 發(fā)動(dòng)機(jī)空空一次表面緊湊換熱器研制,項(xiàng)目負(fù)責(zé)人
2013-2015 發(fā)動(dòng)機(jī)進(jìn)氣系統(tǒng)防冰及結(jié)冰預(yù)測(cè)軟件研制開發(fā)及校驗(yàn),項(xiàng)目負(fù)責(zé)人
2013-2015 渦扇發(fā)動(dòng)機(jī)進(jìn)氣支板滑油防冰技術(shù)研究,項(xiàng)目負(fù)責(zé)人
2013-2015 熱防護(hù)TPS隔熱原理分析及優(yōu)化設(shè)計(jì),項(xiàng)目負(fù)責(zé)人
2013-2014 航空科學(xué)基金重點(diǎn)項(xiàng)目, 進(jìn)氣系統(tǒng)結(jié)冰與冰撞擊適航驗(yàn)證方法研究,合作項(xiàng)目負(fù)責(zé)人
2008-2010 航空科學(xué)基金項(xiàng)目(20081057004)高空臺(tái)混合器-前室傳熱仿真技術(shù)研究,項(xiàng)目負(fù)責(zé)人
2010-2013 燃?xì)廨啓C(jī)中間冷卻器設(shè)計(jì)及試驗(yàn)研究,項(xiàng)目負(fù)責(zé)人
2010-2011 燃機(jī)間冷循環(huán)流動(dòng)換熱與阻力相關(guān)計(jì)算方法研究,項(xiàng)目負(fù)責(zé)人
2007-2011 燃機(jī)中間冷卻器設(shè)計(jì)及試驗(yàn)研究,項(xiàng)目負(fù)責(zé)人
2008-2010 上海航天基金項(xiàng)目,飛行器氣動(dòng)熱精確預(yù)測(cè)方法研究,項(xiàng)目負(fù)責(zé)人
代表性論文專著
1. 董葳,范緒箕, “求解激波/邊界層相互干擾問題的有限體積方法”,上海交通大學(xué)學(xué)報(bào),Vol.32,No.1,pp:140-142, 1998。
2. Wei Dong, H.T.Fan, “Finite Volume TVD Algorithm for Computation of Aerodynamic Heating”, ASME-IMECE,1998.
3. 董葳,范緒箕, “高速粘性繞流的有限體積TVD格式”, 空氣動(dòng)力學(xué)學(xué)報(bào),Vol.17(3),pp.299-304, 1999。
4. 范緒箕,董威, “飛行器突起物周圍氣動(dòng)加熱的計(jì)算方法”,宇航學(xué)報(bào),Vol.19(1),pp.98-102, 1998。
5.Hong Liu, Wei Dong, H.T.Fan, “Conservative and Non-Conservative Overlapping Grid Gernation in Simulating Complex Supersonic Flow”, AIAA -99-3305, 1999.
6. 董葳,范緒箕,"水平蜂窩腔內(nèi)三維自然對(duì)流的數(shù)值計(jì)算",上海交通大學(xué)學(xué)報(bào),Vol.38(10),pp.1631-1634,2004(EI2005028785881).
7.董葳,范緒箕,"熱防護(hù)系統(tǒng)中六角蜂窩內(nèi)的流動(dòng)換熱研究",空氣動(dòng)力學(xué)學(xué)報(bào),Vol.23(4),pp.496-500, 2005(EI2006129772613).
8.董威,黃維娜, “某型高壓渦輪冷卻葉片流動(dòng)換熱的流固耦合計(jì)算研究”,燃?xì)廨啓C(jī)試驗(yàn)與研究,Vol.19(2),pp.14-17,2006。
9.董葳,趙冬梅,“飛行結(jié)冰動(dòng)力學(xué)的研究發(fā)展綜述”,中國(guó)第一屆近代空氣動(dòng)力學(xué)與氣動(dòng)熱力學(xué)會(huì)議論文集,CARS-2006-0-0050,2006。
10.蔣友娣,董葳,陳勇,"高超聲速鈍頭體變熵流表面熱流計(jì)算",航空動(dòng)力學(xué)報(bào),Vol.23(9):1591-1594,2008(EI20084211646749).
11.董威,文超柱,鄭培英. 船用燃?xì)廨啓C(jī)間冷器優(yōu)化設(shè)計(jì)分析[R].云南麗江:中國(guó)航空學(xué)會(huì)第六屆輕型燃?xì)廨啓C(jī)學(xué)術(shù)交流會(huì),2009
12.李會(huì)萍,董葳,“高超聲速再入鈍頭體表面熱流計(jì)算”,上海航天,2010,27(2):18-22。
13.董葳,侯玉柱,閔現(xiàn)花,"進(jìn)口導(dǎo)向葉片熱氣防冰系統(tǒng)試驗(yàn)研究",上海交通大學(xué)學(xué)報(bào),2010,44(11):1579-1582(EI20110113551325).
14.董威,文超柱,鄭培英,"船用燃?xì)廨啓C(jī)間冷器流路的數(shù)值計(jì)算分析",航空動(dòng)力學(xué)報(bào),2010,25(3):636-640(EI20101912918575).
15.董威,石中均,趙秋月,“防冰部件水撞擊特性試驗(yàn)相似準(zhǔn)則分析”,中國(guó)航空動(dòng)力年會(huì),2010
16.文超柱,董威,"艦載燃?xì)廨啓C(jī)間冷器傳熱與流動(dòng)的數(shù)值模擬",航空動(dòng)力學(xué)報(bào),2010,25(3):654-658(EI20133316600208).
17.侯玉柱,鄭京良,董威,"高超聲速飛行器瞬態(tài)熱試驗(yàn)",航空動(dòng)力學(xué)報(bào),2010,25(2):343-347(EI20101412827202).
18. W. Dong, J. J. Zhu, X. H. Min, Calculation of the Heat Transfer and Temperature on the Aircraft Anti-icing Surface, 27th International Congress of the Aeronautical Sciences, 2010(EI20132316406190).
19.董威,高鵬 ,鄭培英,楊芳菲,艦船燃?xì)廨啓C(jī)間冷器優(yōu)化設(shè)計(jì)與性能分析,航空發(fā)動(dòng)機(jī),2011.6
20. W.Dong, J. J. Zhu, Q. Y. Zhao, “Numerical Simulation of the Guide Vane with Hot Air Anti-icing Passage”,42nd AIAA Thermophysics Conference, AIAA-2011-3944,2011(EI20134016806378).
21.Zhu Jian-Jun,Dong Wei,Cai Ying-Lei, “Numerical Study of Water Droplets’ heat and mass transfer characteristics in an entry strut's icing test”,GT2012-68306, 2012(EI20133316600208).
22.Dong Wei, Mao Chun, Zhu Jian-Jun, Chen Yong, “Numerical and experimental analysis of inlet non-uniformity influence on intercooler performance”, GT2012-69231, 2012(EI20133316600437) .
23. Chen Yong, Dong Wei, Parametric Studies Of Nonlinear Damping Behavior Of APS Thermal Barrier Coatings Based On Cohesive Interface Model, GT2012-69343, 2012(EI20133316600732).
24. W. Dong, J. Zhu, Zhixiang Zhou, X. Chi, “Heat Transfer and Temperature Analysis of an Anti-icing System for an Aero-engine Strut under Icing Condition”, AIAA 2012-2753, 2012(EI20133116572878).
25.W. Dong, J. J. Zhu, Y. L. Cai, “The Performance Computation of The Hot Air Anti-icing System Of AN Aero-engine Cone”,28th International Congress of the Aeronautical Sciences, 2012(EI20132416412539).
26.董威,朱劍鋆,周志翔,董奇,"航空發(fā)動(dòng)機(jī)支板滑油防冰性能試驗(yàn)",航空學(xué)報(bào),2014,35(7):1845-1853(EI20143218042412).
27.W. Dong, J. Ding, Zh.X. Zhou, "Experimental Study on the Ice Freezing Adhesive Characteristics of Metal Surfaces",Journal of aircraft,2014,51(3):719-726(SCI000337984100002 EI20142817914563).
28.W. Dong, J. Zhu, M.Zheng and Y.Chen, "Thermal Analysis and Testing of a Cone with Leading Edge Hot Air Anti-icing System",AIAA 2014-0739, 2014(EI20142617874565).
29.W. Dong, J. Zhu, Y. Chen and M. Zheng, "Numerical study of ice accretion on rotating aero-engine cone", 29th Congress of the International Council of the Aeronautical Sciences, 2014.
30.W. Dong, J. Zhu, Y.Chen and M.Zheng, "Numerical analysis of oil anti-icing system performance of turboshaft engine inlet strut", Proceedings of ASME Turbo Expo 2014, GT2014-26564.
31.W. Dong, J. Zhu, Y.Chen and Zhixiang Zhou, "Experimental study on hot lubricating oil anti-icing system of aero-engine strut", Proceedings of ASME Turbo Expo 2014, GT2014-26502.
32.Wei Dong, Jianjun Zhu, Mei Zheng, Rui Wang, "Numerical studies of the water droplet parameters in the icing tunnel test", The 15th International Heat Transfer Conference, IHTC15-8670, 2014, Kyoto, Japan
33.Mei Zheng, Wei Dong, Guilin Lei, Jianjun Zhu,"Study of the flow and heat transfer of water film on hot air anti-icing airfoil surface",The 15th International Heat Transfer Conference, IHTC15-8671, 2014, Kyoto, Japan.
34.W. Dong, J. Zhu,Zhixiang Zhou, X.Chi, "Heat Transfer and Temperature Analysis of an Aero-engine Strut under Icing Condition," Journal of Aircraft, 2015,52(1):216-225(SCI,EI).
35. W. Dong, J. Zhu, M. Zheng, Y.Chen, "Thermal Analysis and Testing of Non-rotating Cone Leading Edge Hot Air Anti-icing System,"Journal of Propulsion and Power,2015,31(1):896-902(SCI,EI).
36. W. Dong, J. Zhu, M. Zheng, G.L. Lei, "Experimental Study on Icing and Anti-Icing Characteristics of Engine Inlet Guide Vanes," Journal of Propulsion and Power,2015,31(5):1330-1337(SCI,EI).
37. J. Zhu,W. Dong,M.Zheng, G.Lei,Q.Zhao, "Numerical Investigation of Heat and Mass Transfer on Inlet Cone under Anti-icing Conditions," Journal of Propulsion and Power,2016,32(3):788-796(SCI,EI).
38. W.Dong, M.Zheng,J.Zhu,G.Lei,"Calculation and Analysis of Runback Water Flow on Anti-Icing Airfoil Surface," Journal of Aircraft, 2016,53(6):1597-1605(SCI,EI).
39. Liu Yinze, Dong Wei, Lei Guilin and Yu Xiao. Numerical Simulation on the Performance of Air-Air Primary Surface Heat Exchanger. ASME Paper GT2016-56905.
40. 鄭梅, 董威, 朱劍鋆,等. 來(lái)流速度對(duì)防冰表面溢流水流動(dòng)換熱的影響. 空氣動(dòng)力學(xué)學(xué)報(bào), 2016, 34(3):295-301.
41. 鄭梅, 朱劍鋆, 董威. 液態(tài)水含量對(duì)防冰表面水膜流動(dòng)換熱的影響. 航空發(fā)動(dòng)機(jī), 2016, 42(1):59-64.
42. 郭宇翔, 劉蔭澤, 董威, 雷桂林, 朱劍鋆. 大水滴撞擊壁面的動(dòng)態(tài)特性數(shù)值模擬. 空氣動(dòng)力學(xué)學(xué)報(bào), 2016, 34(5):573-580.
43.W.Dong, M.Zheng,J.Zhu,G.Lei,Q.Zhao,"Experimental Investigation on Anti-icing Performance of an Engine Inlet Strut," Journal of Propulsion and Power,2017,32(3):379-386(SCI,EI).
44.Lei G L, Dong W, Zheng M, et al. Numerical investigation on heat transfer and melting process of ice with different porosities. International Journal of Heat and Mass Transfer, 2017, 107: 934-944.(SCI,EI).
45. 雷桂林, 鄭梅, 董威,等. 航空發(fā)動(dòng)機(jī)進(jìn)氣支板電熱防冰試驗(yàn)[J]. 航空學(xué)報(bào), 2017, 38(8): 121066.
46. 郭之強(qiáng), 鄭梅, 董威,等. 表面凸起對(duì)機(jī)翼熱氣防冰腔內(nèi)換熱強(qiáng)化的影響[J]. 航空學(xué)報(bào), 2017, 38(2): 520709.
47. 劉蔭澤, 張聲寶, 董威, 劉振宇,于霄, 航空發(fā)動(dòng)機(jī)1次表面換熱器流動(dòng)換熱性能分析[J]. 航空發(fā)動(dòng)機(jī), 2017, 43(4):61-68.
48. M Zheng, W Dong, Z Guo, G Lei. Analysis of Runback Water Flow on Anti-Icing Surface Using Volume-of-Fluid Method. ASME Turbo Expo 2017, June 26-30 ,Charlotte, USA ,ASME Paper GT2017-63933.
49. Z Guo,?M Zheng,?Y Liu,?W Dong. Investigations of Single Jet Impinging on Plates With Circular Dimples. ASME Turbo Expo 2017, June 26-30 ,Charlotte, USA ,ASME Paper GT2017-64052.
50. Dong Wei, Zheng Mei, Guo Zhiqiang, Lei Guilin, Numerical Investigation of the Heat and Mass Transfer on Anti-icing Surface, CHT-17: ICHMT International Symposium on Advances in Computational Heat Transfer, 2017, May 28 - June 01 Napoli, Italy.
51. 雷桂林, 鄭梅, 董威,等. 積冰密度對(duì)機(jī)翼除冰過程影響的數(shù)值研究[J]. 空氣動(dòng)力學(xué)學(xué)報(bào), 2018, 36(6): 958-965.
52. Zheng M, Wu T, Guo Z, et al. Calculation of Water Film Flow and Heat Transfer on the Aircraft Anti-icing Surface[C]. 31st Congress of the International Council of the Aeronautical Sciences, 2018.
53. Wu T, Yang Q, Guo Z, et al. Supercooled Water Droplet Impingement and Icing Region Prediction on a Rotating Fan Blade[C]//AIAA Aviation 2019 Forum. 2019: 3309.
54. Yang Q, Guo Z, Zheng M, et al. The Effect of Crosswinds on Icing at Turbofan Engine Inlet[C]. SAE Technical Paper, 2019.
55. 鄭梅, 鄭莉, 郭之強(qiáng), 等. 結(jié)冰風(fēng)洞云霧參數(shù)不同測(cè)量手段的試驗(yàn)對(duì)比[J]. 空氣動(dòng)力學(xué)學(xué)報(bào), 2019, 37(6): 983-989.
56. 姜飛飛, 董威, 鄭梅, 等. 冰晶在渦扇發(fā)動(dòng)機(jī)內(nèi)相變換熱特性[J]. 航空動(dòng)力學(xué)報(bào), 2019, 34(3): 567-575.
57. 楊倩, 董威, 郭之強(qiáng), 等. 渦扇發(fā)動(dòng)機(jī)短艙結(jié)冰試驗(yàn)相似方法[J]. 航空動(dòng)力學(xué)報(bào), 2019, 34(9): 1988-2000.
58. Zheng M, Guo Z, Dong W, et al. Experimental investigation on ice accretion on a rotating aero-engine spinner with hydrophobic coating[J]. International Journal of Heat and Mass Transfer, 2019, 136: 404-414. (SCI,EI)
59. Yang X, Yang Q, Dong W. Aeroengine data reconciliation model based on cooperative working equations[J]. Energy, 2019, 186: 115914. (SCI,EI)
60. Yang X, Dong W, Yang Q, et al. Withdrawal: A Simplified Model for the Simulation of Synergistic Air-Breathing Rocket Engine[C]// AIAA Propulsion and Energy 2019 Forum. 2019.
61. Guo X, Guo Z, Yang Q, et al. Numerical Simulation Model of Electrothermal De-Icing Process on Composite Substrate[C]//Turbo Expo: Power for Land, Sea, and Air. ASME, 2020, 84072: V02BT34A017.
62. Yang X, Guo X, Dong W. On-Line Component Map Adaptive Procedure Based on Sensor Data[C]//Turbo Expo: Power for Land, Sea, and Air. ASME, 2020, 84058: V001T01A041.
63. 楊學(xué)森, 楊橋, 張韋雅, 等. 某型渦扇發(fā)動(dòng)機(jī)測(cè)量數(shù)據(jù)融合模型[J]. 航空動(dòng)力學(xué)報(bào), 2020, 35(3). (EI)
64. 蔡學(xué)成, 李芹, 楊學(xué)森, 等. 旋轉(zhuǎn)對(duì)沖擊射流流動(dòng)及換熱影響的數(shù)值研究[J]. 航空動(dòng)力學(xué)報(bào), 2021. (EI)
65. 李芹,楊肖峰,董威,杜雁霞.高超聲速飛行器表面吸附特性對(duì)多相催化過程影響的數(shù)值模擬[J].上海交通大學(xué)學(xué)報(bào),2021,55(11):1352-1361.DOI:10.16183/j.cnki.jsjtu.2020.288.
66. Guo Z, Zheng M, Yang Q, et al. Effects of flow parameters on thermal performance of an inner-liner anti-icing system with jets impingement heat transfer [J]. Chinese Journal of Aeronautics, 2021. (SCI,EI)
67. Jian M, Yang X, Dong W. Numerical Investigation on the Flow Characteristics in a Cover-Plate Pre-Swirl System[C]//Turbo Expo: Power for Land, Sea, and Air. ASME, 2021, 84942: V03AT04A042.
68. 李治達(dá),陳翔翔,吳濤,董威.高效彎掠對(duì)轉(zhuǎn)槳扇流動(dòng)特點(diǎn)與槳距調(diào)節(jié)規(guī)律[J].航空動(dòng)力學(xué)報(bào):1-11[2022-08-01].DOI:10.13224/j.cnki.jasp.20210278.
69. 陳翔翔,李治達(dá),李芹,鄭浩冉,董威.基于LBM的發(fā)汗孔隙結(jié)構(gòu)內(nèi)流動(dòng)換熱性能[J].航空動(dòng)力學(xué)報(bào):1-10[2022-08-01].DOI:10.13224/j.cnki.jasp.20210425.
70. Wei H, Li Z, Guo X, et al. Experimental study on the influence of airflow velocity on frosting and defrosting performance of compact precooler under actual air humidity condition[J]. International Journal of Heat and Mass Transfer, 2022, 184: 122284. (SCI,EI)
71. Guo Z, Guo X F, Yang Q, et al. Heat transfer characteristics of unexpanded jet impingement in piccolo hot air anti-icing chamber[J]. Applied Thermal Engineering, 2022, 200: 117540. (SCI,EI)
72. Yang X, Jian M, Dong W, et al. Simulation of the secondary air system of turbofan engines: Insights from 1D-3D modeling[J]. Chinese Journal of Aeronautics, 2022. (SCI,EI)
73. Yang Q, Guo X, Dong W, et al. Ice accretion and aerodynamic effects on a turbofan engine nacelle under takeoff conditions[J]. Aerospace Science and Technology, 2022. (SCI,EI)
74. 楊倩,郭曉峰,李芹,董威. 基于POD和代理模型的熱氣防冰性能預(yù)測(cè)方法[J]. 航空學(xué)報(bào), 2022. doi: 10.7527/S1000-6893.2022.26992.
75. Wei H, Guo X, Li Z, et al. Experimental investigation on effects of freestream humidity on the frosting and defrosting characteristics of microtubule precooler[J]. Applied Thermal Engineering, 2022, 206: 118104. (SCI,EI)
軟件版權(quán)登記及專利
軟件著作權(quán):一次表面空空換熱器計(jì)算軟件,2015SR180881
軟件著作權(quán):航空發(fā)動(dòng)機(jī)進(jìn)氣部件防冰性能分析軟件平臺(tái),2016SR155591
軟件著作權(quán):冰風(fēng)洞水霧參數(shù)計(jì)算分析軟件,2016SR273332
專利:可瞄準(zhǔn)的電子控制式鳥彈撞擊試驗(yàn)裝置,ZL2014-1-0131276.3
專利:渦輪風(fēng)扇發(fā)動(dòng)機(jī)進(jìn)口部件鳥彈撞擊裝置,ZL2014-1-0131279.7
專利:雙冷庫(kù)循環(huán)的結(jié)冰與防冰試驗(yàn)裝置,ZL2015-1-0133720.X
專利:航空發(fā)動(dòng)機(jī)進(jìn)氣道支板的防冰系統(tǒng)及防冰方法,ZL2016-1-0248452.0
1999 部級(jí)科學(xué)技術(shù)進(jìn)步一等獎(jiǎng)
2011 湖南省國(guó)防科技進(jìn)步獎(jiǎng)二等獎(jiǎng)