崔涛 - 浙江大学 - 航空航天学院

个人简介

崔涛，浙江大学航空航天学院教授，航空宇航科学与技术、力学专业博士生导师。在哈尔滨工业大学获得学士、硕士和博士学位并留校任教。曾分别在国防科学技术大学、Washington University in St. Louis作博士后及访问学者。主要研究方向为流动燃烧机理、非线性动力学与控制、空天动力系统。在教学和研究生培养过程中，注重从认识论出发建立知识的可理解性与认知信心。注重追溯抽象概念中的直观概念，注重构造从直观到演绎的认知序，注重对概念和逻辑体系的语言表达。在科研过程中，注重从集合论出发来构造发动机中的集合及其几何与代数结构，以探索复杂变化中的不变性质和量化方法。主持多项国家自然科学基金、国家重大科技专项项目，在行业内著名期刊AIAA J., AIAA J. Propulsion and Power, AIAA J. Aircraft发表多篇论文，获得教育部科技进步一等奖、国防技术发明二等奖各一项。欢迎合作开展博士后研究，要求申请人具有航空宇航科学与技术、动力工程及工程热物理、流体力学、燃烧学、控制或与空天动力系统相关的物理、力学等专业背景。获奖情况鲍文, 崔涛, 常军涛, 秦江, 周伟星, 于达仁, 唐井峰，牛文玉. XXX发动机控制技术，教育部科技进步奖，一等，2016.3. 基金项目国家自然科学基金面上项目，51976182，运动激波稳定在超声速进气道喉道的设想及原理探索，2020/01-2023/12、主持。国家自然科学基金重大研究计划项目，91541106，超声速燃烧室理想释热规律与理想几何构型的探索，2016/01-2018/12、主持。国家自然科学基金面上项目，51476041，基于离散化思想的吸气式冲压发动机进气道再起动控制问题研究方法，2015/01-2018/12、主持。国家自然科学基金面上项目，11072071，激波反射模式转变的迟滞回路耦合规律研究，2011/01-2013/12、主持。国家自然科学基金青年基金项目，50906015，一种进气道起动/不起动边界建模的拓扑学方法，2010/01-2012/12、主持。国家重大科技专项项目，XXX发动机加减速控制，2018/09-2021/12，主持。国家重大科技专项项目，XXX释热规律及转换机理研究，2010/01-2010/12，主持。

研究领域

流动燃烧机理；非线性动力学与控制；空天动力系统

近期论文

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论文和专著 Zhuang Ma, Gaofeng Wang, Tao Cui*, Yao Zheng. Interpretation of Intermittent Combustion Oscillations by a New Linearization Procedure. AIAA Journal of Propulsion and Power, accepted. Zhuang Ma, Tingwei Ji, Tao Cui*, Yao Zheng. Access to Empirical Formulations of Combustion Efficiency for Gas Turbine Combustors with Improved Generalization Ability. ASME Journal of Thermal Science and Engineering, accepted. Xinyue Hao, Tao Cui, Kai Liu, Daren Yu, Zexu Zhang. Behavior Sequence(s) of Ramjets and Uncontrollable Problems Due to Undesired Behavior Categories. AIAA Journal, Vol. 57, No. 5, 2019: 2227-2236. Shengbo Yang, Tao Cui, Xinyue Hao, Daren Yu. Ideal Heat Release and Ideal Inner Configuration of Supersonic Combustor. AIAA Journal of Propulsion and Power, Vol. 34, No. 2, 2018: 374-383. Ruifeng Cao, Tao Cui*, Daren Yu, Juntao Chang, Wen Bao, and Zhongqi Wang. New Method for Solving One-Dimensional Transonic Reacting Flows of a Scramjet Combustor. AIAA Journal of Propulsion and Power, Vol. 32, No. 6, 2016: 1403-1412. Tao Cui*, Yong Wang, Kai Liu, Jianren Jin. Classification of Combustor-Inlet Interactions for Air-Breathing Ramjet Propulsion. AIAA Journal. Vol. 53, No. 8, 2015: 2237-2255. Tao Cui*, Yong Wang, Daren Yu. Bistability and Hysteresis in a Nonlinear Dynamic Model of Shock Motion. AIAA Journal of Aircraft, Vol. 51, No. 5, 2014: 1373-1379. Tao Cui*, Shunlin Tang. Geometry Rule of Combustor-Inlet Interaction in Ramjet Engines. AIAA Journal of Propulsion and Power, Vol.30, No.2, 2014: 449-460. Tao Cui*, Shengbo Yang, Daren Yu. Ideal Heat Release of Supersonic Combustion, AIAA Journal of Propulsion and Power, Vol.29, No.3, 2013: 621-627. Tao Cui, Xuegang He, Daren Yu*, Shunlin Tang. Multistability and Loops-Coupled Hysteresis: Flight-Test Analysis on Error Detection of Inlet Start/Unstart. AIAA Journal of Propulsion and Power, Vol.28, No.3, 2012: 496-503. Tao Cui*, Shunlin Tang, Chao Zhang, Daren Yu. Hysteresis Phenomenon of Mode Transition in Ramjet Engines and Its Topological Rule. AIAA Journal of Propulsion and Power, Vol. 28, No. 6, 2012: 1277-1284. Tao Cui*, Zhong Lv, Daren Yu. Multi-Stability and Complex Routes of Supersonic Inlet Start/Unstart. AIAA Journal of Propulsion and Power, Vol. 27, No. 6, 2011: 1204-1211. Tao Cui*, Daren Yu, Juntao Chang, Wen Bao. Catastrophe Model for Supersonic Inlet Start/Unstart. AIAA Journal of Aircraft, Vol. 46, No. 4, 2009: 160-1166. Tao Cui*, Daren Yu, Juntao Chang, Wen Bao. Topological Geometry Interpretation of supersonic Inlet Start/Unstart Based on Catastrophe Theory. AIAA Journal of Aircraft, Vol. 45, No.4, 2008: 1464-1468. Daren Yu, Tao Cui*, Wen Bao. Equilibrium Manifold Linearization Model for Normal Shock Position Control Systems. AIAA Journal of Aircraft, Vol.42, No.5, 2005: 1344-1347. Tao Cui*, Shunlin Tang, Lei Zhang, Daren Yu. Swallowtail Model for Predicting the Global Bifurcation Behaviors of CO Oxidation Reaction, Science in , Series B, Vol.54, No.7, 2011: 1072–1077. Daren Yu*, Tao Cui, Wen Bao. Catastrophe, hysteresis and bifurcation of mode transition in scramjet engines and its model. Science in , Series E, 2009, Vol. 52, No. 6, 2009: 1543-1550. Tao Cui*, Xiaoliang Jiao, Daren Yu. Geometry of the Transition Criterion of Shock Wave Reflection over a Wedge. Shock Waves, Vol. 25, No. 1, 2015: 23-34. Tao Cui*, Daren Yu, Wen Bao. Distributed Parameter Control Arithmetic for an Axisymmetrical Dual-mode Scramjet. Aeronautical Journal, Vol. 112, No.1135, 2008: 557-565. Daren Yu, Tao Cui*, Wen Bao. An Idea of Distributed Parameter Control for Scramjet Engines. Aeronautical Journal, Vol. 111, No.1126, 2007:787-796. 崔涛, 于达仁. 吸气式冲压发动机突变动力学与控制. 科学出版社, 北京, 2016.