屈峰


的个人主页 http://teacher.nwpu.edu.cn/196CFFC38566437DA26E703774169C63

  被浏览次数:13528

基本信息 The basic information

屈峰

航空学院

博士研究生毕业

工学博士

副教授

航空宇航科学-飞行器设计,力学-流体力学,力学-空气动力学

qufeng@nwpu.edu.cn

工作经历 Work Experience

(1) 2018.1-至今, 西北工业大学, 航空学院, 副教授

(2) 2015.8-2017.12, 中国空间技术研究院, 载人航天总体部, 工程师 

荣誉获奖 Awards Information

2021:西北工业大学“翱翔新星”

2021:西北工业大学青年人才培育计划入选者

2020:中国航空学会科学技术二等奖(排名第一)

2020:全国流体力学大会优秀论文

2019:第五届中国科协青年人才托举工程


科学研究 Scientific Research

     

屈峰,博士生导师,长期从事先进飞行器总体气动设计技术以及复杂流动高精度数值模拟方法研究。曾任职于中国空间技术研究院载人航天总体部,作为总体设计师承担载人飞船以及新一代天地往返运输系统的总体气动设计工作。先后主持JCJQ重点项目、GF创新特区项目、XX国家科技重大专项子课题、国家自然科学基金面上项目、相关国家重点型号关键技术攻关等课题10余项。以第一或通讯作者身份在国内外领域顶级期刊正式发表高水平学术论文30余篇(JCR一区21篇)。获2020年度中国航空学会科学技术二等奖(排名第一),入选第五届中国科协青年人才托举工程,受聘任《International Journal of Aerospace Engineering》期刊专栏特邀主编、《力学与实践》期刊编委、《气动研究与实验》青年编委、《航空学报》“先进天地往返系统气动设计研究”专栏客座编辑。现为中国航空学会空气动力学分委会委员,并担任多项国际、国内学术会议的分会主席或技术委员会成员。



近年所主持科研项目:

1.       XX综合设计技术研究,XX基础加强重大研究计划重点课题(国家级),主持,2020.05-2022.10

2.       前体/进气道高精度气动热仿真方法研究XX基础加强重大研究计划课题(国家级),2021.01-2021.12

3.       面向高速飞行器复杂流动模拟的真正多维全速域黎曼通量求解方法研究,国家自然科学基金面上项目(国家级),主持,2020.01 - 2023.12

4.       第五届中国科协青年人才托举工程,主持,2019.01-2021.12

5.       涡桨飞机气动噪声精细化预测技术研究,工信部XX科技专项(国家级),主持,2018.01-2020.12

6.       XXXX关键技术研究,XX创新特区项目(国家级),主持,2020.05-2021.12

7.       基于伴随的双后掠乘波体气动优化设计,国防科工局XX企业稳定支持项目子课题(国家级),主持,2020.01-2021.12

8.       基于全速域空间离散格式及伴随方法的高超声速飞行器优化设计方法,陕西省自然科学基金一般项目(省部级),主持,2019.01-2020.12

9.       某跨域飞行器长时滞空气动布局设计与优化研究,XX院所横向课题,主持,2021.07-2022.07

10.   高速飞行器一级外形方案优化设计,XX院所横向课题,主持,2019.01-2020.01

11.   组合体融合体乘波体气动布局研究,XX院所横向课题,主持,2019.01-2020.01

12.   宽速域飞行器水平起降增稳增效气动布局优化设计技术研究,XX院所横向课题,主持,2020.11-2021.11

13.   机翼吹气技术研究XX院所横向课题主持,2020.01-2020.06

14.   面向宽速域飞行器优化设计的高效优化算法, 国防科工局基础科研项目子课题(国家级),主要参与人,2019.11-2021.12

15.   高低速兼顾的扁平翼身融合体布局优化设计研究XX院所横向课题,主要参与人,2020.01-2020.06



研究方向:

(1)计算流体力学

(2)飞行器设计 

(3)高超声速空气动力学



学术成果 Academic Achievements

代表性文章:

2021

[1]     B. X. Zhou, F. Qu, D. Sun, Z.R Wang, J. Q. Bai, A study of higher-order reconstruction methods for genuinely two-dimensional Riemann solver, Journal of Computational Physics, 2021, 443, 110469. (唯一通讯作者,中科院I区,Top期刊)

[2]     F. Qu, D. Sun, Q. S. Liu, J. Q. Bai, Low-speed modification for the genuinely multidimensional Harten, Lax, van Leer and Einfeldt Scheme in curvilinear coordinates, Journal of Scientific Computing, 2021. (唯一第一作者,中科院II)

[3]     D. Sun, F. Qu, Q. S. Liu, J. Zhong, Improvement of the genuinely multidimensional ME-AUSMPW scheme for subsonic flows, Computers and Mathematic with applications, 2021, 96, 1-15. (唯一通讯作者,中科院I区,Top期刊)

[4]     F. Qu, D. Sun, J. Q. Bai, A hybrid multidimensional Riemann solver to couple the self-similar method with the MULTV method for complex flows, Chinese Journal of Aeronautics, 2021, 34(7), 29-38. (唯一第一作者,中科院II)

[5]     J. Chen, F. Qu, X. Wu, Z. Wang, J. Bai, Numerical study of interactions between shock waves and a circular or elliptic bubble in air medium, Physics of Fluids, 2021, 33 (4), 043301. (唯一通讯作者,中科院I区,Top期刊)

[6]     D. Sun, F. Qu, J. Q. Bai, Numerical Study of the suction flow control of the supersonic boundary layer transition in a framework of gas-kinetic scheme, Aerospace science and technology, 2021, 109, 106397. (唯一通讯作者,中科院I区,Top期刊)

[7]     E. Lu, L. Zuo, Z. Guo, H. Zeng, W. Zhu, F. Qu, Preliminary study on heat flux measurement data of TT-0 flight test, Chinese Journal of Aeronautics, 2021, 34(5), 120-128. (唯一通讯作者,中科院II)

[8]     H. Wang, R. Ji, F. Qu, J. Q. Bai, Q. Fu, H. Li, Three-dimensional pore-scale study of the directional heat transfer in a high thermal conductivity carbon/carbon composite protection system, Aerospace science and technology, 2021, 112, 106609. (中科院I区,Top期刊)

[9]     M. Li, J. Q. Bai, F. Qu, Radar cross section reduction and shape optimization using adjoint method and automatic differentiation, Applied Computational Electromagnetics Society Journal, 2021, 36, 320-335.

[10] 张宇佳,左光,徐艺哲,杜若凡,赵飞,屈峰,Starship新型舵面形式气动特性数值模拟,航空学报,2021,42,624058.

 

2020

[11] F. Qu, D. Sun, B. X. Zhou, J. Q. Bai, Self-similar structures based genuinely two-dimensional Riemann solvers in curvilinear coordinates, Journal of Computational Physics, 2020, 109668. (唯一第一作者,中科院I区,Top期刊)

[12] D. Sun, F. Qu, J. Q. Bai, C. Yan, An effective low dissipation method for compressible flows, Aerospace science and technology, 2020, 100, 105757. (唯一通讯作者,中科院I区,Top期刊)

[13] Y. Shi, T. Cao, T. Yang, J. Q. Bai, F. Qu, Y. Yang, Estimation and analysis of hybrid laminar flow control on a transonic experiment, AIAA Journal, 2020, 58, 118-132.

[14] 阎超,屈峰,赵雅甜,于剑等,航空航天CFD物理模型和计算方法的述评与挑战,空气动力学报,2020,38,829-857.

 

2019

[15] F. Qu, D. Sun, J. Q. Bai, C. Yan, A genuinely two-dimensional Riemann solver for compressible flows in curvilinear coordinates, Journal of Computational Physics, 2019, 386, 47-63. (唯一第一作者,中科院I区,Top期刊)

[16] F. Qu, D. Sun, J. Q. Bai, A new genuinely two-dimensional Riemann solver for multidimensional Euler and Navier - Stokes Equations, Computer Physics Communications, 2019, 243, 1-11. (唯一第一作者,中科院I区,Top期刊)

[17] F. Qu, J. J. Chen, D. Sun, J. Q. Bai, G. Zuo, A grid strategy for predicting the space planes hypersonic aerodynamic heating loads, Aerospace science and technology, 2019, 86, 659-670. (唯一第一作者,中科院I区,Top期刊)

[18] F. Qu, D. Sun, K. Han, J. Q. Bai, G. Zuo, C. Yan, Numerical investigation of the supersonic stabilizing parachute’s heating loads, Aerospace science and technology, 2019, 87, 89-97. (唯一第一作者,中科院I区,Top期刊)

[19] F. Qu, W. X. Kong, D. Sun, J. Q. Bai, Shock-stable flux scheme for predicting the hypersonic airliner’s aerodynamic heating loads, Science China Physics, Mechanics & Astronomy,2019, 62 (8), 984711. (唯一第一作者,中科院I区,Top期刊)

[20] F. Qu, J. J. Chen, D. Sun, J. Q. Bai, C. Yan, A new all-speed flux scheme for the Euler equations, Computers and Mathematic with applications, 2019, 77, 1216-1231. (唯一第一作者,中科院II区,Top期刊)

 

2018

[21] Qu, F.,Sun, D.,Zuo, G., A study of upwind schemes on the laminar hypersonic heating predictions for the reusable space vehicle, Acta Astronautica, 2018, 147, 412-420. (唯一第一作者,中科院II)

[22] Feng Qu, Di Sun, Chao Yan, A new flux splitting scheme for the Euler equations II: E-AUSMPWAS for All Speeds, Communications in Nonlinear Science and Numerical Simulation, 2018, 57, 58-79. (唯一第一作者,中科院I区,Top期刊)

[23] F. Qu, D. Sun, J. Q. Bai, G. Zuo, et al, Numerical investigation of blunt body’s heating load reduction with combination of spike and opposing jet, International Journal of Heat and Mass Transfer, 2018, 127, 7-15. (唯一第一作者,中科院I区,Top期刊)

[24] Sun, D.,Qu, F.,Yan, C., An effective flux scheme for hypersonic heating prediction of re-entry vehicles, Computers and Fluids, 2018, 176, 109-116. (唯一通讯作者,中科院III)

[25] R. F. Du, C. Yan, F. Qu, L. Zhou, Investigation of all-speed schemes for turbulent simulations with low-speed features, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232, 757-770.

[26] 陈鑫,左光,屈峰,陈冲,自备动力逃逸载人飞船上升段气动特性研究,航天器工程,2018(1)

 

2017

[27] Qu, F.,Sun, D., Investigation into the influences of the low-speed flows’ accuracy on RANS simulations, Aerospace Science and Technology, 2017, 70, 578-589. (唯一第一作者,中科院I区,Top期刊)

[28] Qu, F.,Sun, D.,Zuo, G.,Shi, Y., An improvement on the AUSMPWM scheme for hypersonic heating predictions, International Journal of Heat and Mass Transfer, 2017, 108, 2492-2501. (唯一第一作者,中科院I区,Top期刊)

[29] 左光,和宇硕,石泳,屈峰,X-37B飞行器气动力辅助异面变轨性能研究,航天返回与遥感,2017(38).

 

2016年及以前

[30] Sun, D.,Qu, F.,Yan, C., An efficient adaptive high-order scheme based on the WENO process, Computers and Fluids, 2016, 140, 81-96. (唯一通讯作者,中科院III)

[31] Qu, F.,Yan, C.,Sun, D., Investigation into the influences of the low speed's accuracy on the hypersonic heating computations, International Communications in Heat and Mass Transfer, 2016, 70, 53-58. (唯一第一作者,中科院I区,Top期刊)

[32] Qu, F., Yan, C., Sun, D., Jiang, Z., A new Roe-type scheme for all speeds, Computers and Fluids, 2015, 121, 11-25. (唯一第一作者,中科院II)

[33] Feng Qu, Chao Yan, Di Sun. A Parameter-free scheme for all speeds’simulations. Science China Technological Sciences, 2015, 58, 434-442. (唯一第一作者,中科院II)

[34] Feng Qu, Chao Yan, Jian Yu, Di Sun. A new flux splitting scheme for the Euler equations. Computers and Fluids, 2014, 102, 203-214. (唯一第一作者,中科院II)

[35] Feng Qu, Chao Yan, Jian Yu, Di Sun. A study of parameter-free shock capturing upwind schemes on low speeds’issues. Science China Technological Sciences, 2014, 57, 1183-1190. (唯一第一作者,中科院II)

[36] Jiang, Z., Yan, C., Yu, J., Qu, F., Ma, L., Effective high-order solver with thermally perfect gas model for hypersonic heating prediction, Applied Thermal Engineering, 2016, 99, 147-159.

[37] Feng Qu, Chao Yan, Jian Yu, Chongyan Zhong. Construction of shock stable scheme based on RoeM scheme. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40: 613-617. (in Chinese)

[38] Feng Qu, Chao Yan, Jian Yu, Jiayang Chen. Assessment of shock capturing methods for numerical simulations of compressible turbulence with shock waves. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40: 1085-1089. (in Chinese)



社会兼职 Social Appointments

中国航空学会空气动力学分会委员 

国家xxxxx项目主任

International Journal of Aerospace Engineering专栏特邀主编 

《力学与实践》期刊编委 

《气动研究与实验》青年编委

翼型、叶珊空气动力学国防科技重点实验室固定人员 

航空学报“先进天地往返系统气动设计研究”专栏客座编辑