2000.02-2003.05上海交通大學博士
1997.09-2000.02上海理工大學碩士
1992.09-1996.07華東工業(yè)大學學士

2003.05- 上海交通大學 機械與動力工程學院 工程熱物理研究所 講師/副教授
2011.02-2012.02 UCDavis Mepartment of aerospace 訪問學者

葉輪機械內部流動
非穩(wěn)定流動
風能利用

中國動力工程學會透平專委會副主任委員
中國電工技術學會新能源發(fā)電設備專委會委員
中國動力工程學會新能源設備專委會委員

橫向, 高溫冷卻葉片流熱耦合分析, 2025-2026, 主持

橫向, 末級葉片振動特性電渦流測試算法開發(fā), 2025-2026, 主研

兩機科學中心項目，2022-2024，課題負責人
兩機項目，，2022-2025，課題負責人
重點研發(fā)計劃, 700℃等級高效超超臨界發(fā)電技術（課題4中的子課題1）, 2018-2021, 子課題主持
橫向, 汽輪機靈活性改造低壓缸低負荷工況安全性研究, 2018-2021, 主持
橫向, 超超臨界汽輪機中壓缸內部主要腔體的流動和換熱問題研究, 2014-2017, 主持
橫向,超超臨界汽輪機中壓缸內部主要腔體的流動和換熱問題研究, 2014-2016, 主持其他, AXXX, 離心壓氣機****數(shù)值研究, 2013-2014, 主持,
橫向, 低壓末三級通流特性分析及動葉強度振動研究, 2014-2015, 主持,  

[1] Shi L, Zhu X, Du Z. Study on convective heat transfer characteristics of inclined jet impinging cylindrical target surface in the confined space [J]. Applied Thermal Engineering, 2023, 218: 119316.
[2] Shi L, Zhu X, Du Z. Study on flow structure and heat transfer mechanism of inclined jet impinging on the rotating cylindrical target surface in the confined space [J]. International Journal of Heat and Mass Transfer, 2023, 216: 124544.
[3] Lian B, Tong X, Zhu X, Du Z, Cui Y, Khoo B C. Investigations on the effects of structural damping on vortex-induced vibration response of an airfoil at a high angle of attack via the aero-damping map[J]. Physics of Fluids, 2023, 35(6): 064107.
[4] Lian B, Tong X, Zhu X, Du Z, Cui Y, Khoo B C. Investigations on lock-in vortex-induced vibration of an airfoil at a high angle of attack based on detached eddy simulation [J]. Physics of Fluids, 2023, 35(9): 094105.
[5] Tian T, Sun C, Zhu X, Du Z. Flow modal decomposition of a vertical-axis wind turbine with the moving boundaries of rotating blades[J]. Journal of Engineering for Gas Turbines and Power, 2022, 144(1): 111003.
[6] Shi L, Sun C, Zhu X, Du Z. A confined laminar slot impinging jet at low Reynolds numbers: unsteady flow and heat transfer characteristics [J]. Journal of Thermal Science, 2023, 32(2): 753-769.
[7] Shi L, Zhu X, Du Z. Experimental investigation on convective heat transfer of inclined jets impinging on the rotating cylindrical surface in the confined space [J]. International Journal of Heat and Mass Transfer, 2022, 202: 123744.
[8] Lian B, Zhu X, Du Z. Numerical study on vortex-induced vibration of wind turbine airfoil at high angle of attack via free vibration simulation[J]. Journal of Renewable and Sustainable Energy, 2022, 14(3): 033306.
[9] Sun C, Tian T, Zhu X, Ouyang H, Du Z. Investigation of the near wake of a horizontal-axis wind turbine model by dynamic mode decomposition [J]. Energy, 2021, 227: 120418.
[10] Zhu X, Sun C, Ouyang H, Du Z. Numerical investigation of the effect of towers and nacelles on the near wake of a horizontal-axis wind turbine model [J]. Energy, 2021: 121782.
[11] Hu P, Lin T, Yang R, Zhu X, Du Z. Numerical investigation on flow instabilities in low-pressure steam turbine last stage under different low-load conditions[J]. Proceedings of the Institution of Mechanical Engineers. Part A: J. Power and Energy, 2021, 235(6):1544-1526.
[12] Hu P, Sun C, Zhu X, Du Z. Investigations on vortex-induced vibration of a wind turbine airfoil at a high angle of attack via modal analysis[J]. Journal of Renewable and Sustainable Energy, 2021, 13(3):033306.
[13] Zhu X, Hu P, Lin T, Du Z. Numerical investigations on non-synchronous vibration and frequency lock-in of low-pressure steam turbine last stage[J]. Proceedings of the Institution of Mechanical Engineers. Part A: J. Power and Energy, 2021, 236(4): 647-661.
[14] Sun C, Tian T, Zhu X, Du Z. Sparse identification of nonlinear unsteady aerodynamics of the oscillating airfoil [J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 235(7): 809-824.
[15] Sun C, Tian T, Zhu X, Du Z. Input-output reduced-order modeling of unsteady flow over an airfoil at a high angle of attack based on dynamic mode decomposition with control [J]. International Journal of Heat and Fluid Flow, 2020, 86(5):108727.
[16] Shi L, Sun C, Zhou D, Zhu X, Du Z. Numerical study of unsteady flow and heat transfer of circular tangential direction jets flowing over the inner cylinder surface in the annular chamber [J]. International Journal of Heat and Fluid Flow, 2020, 85(7): 108648.
[17] 田甜,孫翀,竺曉程,杜朝輝.垂直軸風力機尾跡的時空特性[J].動力工程學報,2023,43(03):341-348+371.
[18] 連波,胡平,竺曉程,杜朝輝.大攻角翼型的鎖頻現(xiàn)象及氣彈穩(wěn)定性研究[J].工程熱物理學報,2023,44(03):668-676.
[19] 孫翀,田甜,竺曉程,杜朝輝.風力機翼型非定常流場POD和EPOD分析[J].上海交通大學學報,2022,56(01):45-52.
[20] 朱能杰,竺曉程,沈昕,杜朝輝.透平葉柵非軸對稱端壁優(yōu)化目標比較[J].熱能動力工程,2022,37(01):41-48.
[21] 何磊,陳大為,張祎,王海峰,劉釗,竺曉程,杜朝輝.透平靜葉表面多排孔氣膜冷卻特性試驗研究[J].動力工程學報,2021,41(12):1040-1044+1068.
[22] 孫翀,田甜,竺曉程,歐陽華,杜朝輝.基于大渦模擬下風力機翼型非定常轉捩流動的動態(tài)模態(tài)分解分析[J].工程熱物理學報,2021,42(12):3156-3163.
[23] 朱能杰,張方,竺曉程,沈昕,杜朝輝.高壓透平動葉非軸對稱端壁優(yōu)化設計[J].熱力透平,2021,50(04):270-275.
[24] 何磊,李月茹,竺曉程,杜朝輝.基于流熱耦合的燃氣輪機透平葉頂冷卻設計[J].熱能動力工程,2021,36(10):27-32.
[25] 張赫輝,薛翔,竺曉程,杜朝輝.基于本征正交分解的無葉擴壓器流動穩(wěn)定性Galerkin降階模型[J].熱能動力工程,2021,36(08):16-21.
[26] 孫翀,石磊,沈昕,竺曉程,杜朝輝.風力機翼型在失速工況下非定常流場的本征正交分解分析[J].工程熱物理學報,2021,42(04):894-904.
[27] 石磊,周代偉,竺曉程,杜朝輝.基于流熱耦合方法的中壓腔渦流冷卻效果數(shù)值研究[J].熱能動力工程,2021,36(01):24-32.
[28] 吳蔚,趙博,薛翔,竺曉程,王彤,杜朝輝.離心壓氣機不穩(wěn)定流動的時頻特征分析[J].航空動力學報,2020,35(08):1768-1776.

[1]  陳進格,沈昕,竺曉程,杜朝輝, 一種基于氣彈模型的風力機葉片預彎預扭設計方法, CN 109902384 B, 發(fā)明專利, 2023.6授權
[2]景瀟，殷承良，馬邦彥，張赫輝，竺曉程，用于無葉擴壓器壁面的類鯊魚皮二維鋸齒狀溝槽結構, 發(fā)明專利, 2023.12授權
[3]趙奕博，景瀟，馬邦彥，竺曉程，壓氣機氣動聲學一體化優(yōu)化設計軟件，2023.7授權
楊曉建,竺曉程,沈昕,胡晨星,孫翀,杜朝輝. 凹槽阻流結構[P]. 上海：CN107061356A,2017-08-18.
[4]  王廣,沈昕,陳進格,竺曉程,杜朝輝. 利用分形維數(shù)測量風場地表粗糙度的方法[P]. 上海：CN106909707A,2017-06-30.
[5]  楊曉建,竺曉程,沈昕,胡晨星,孫翀,杜朝輝. 鋸齒阻流結構[P]. 上海：CN106837858A,2017-06-13.
[6]  楊曉建,竺曉程,沈昕,胡晨星,孫翀,杜朝輝. 帶有環(huán)形突起結構的新型離心壓氣機[P]. 上海：CN106640754A,2017-05-10.
[7]  劉亮亮,竺曉程,劉昊,沈昕,杜朝輝. 受限空間內有橫流的射流沖擊控制結構[P]. 上海：CN106014487A,2016-10-12.