Jun-tao Chang

发表

Modeling and analysis for integrated airframe/propulsion control of vehicles during mode transition of over-under Turbine-Based-Combined-Cycle engines

Daren Yu, Juntao Chang, Jialin Zheng, 2019 .

One-day-ahead probabilistic wind speed forecast based on optimized numerical weather prediction data

Daren Yu, Jinfu Liu, Juntao Chang, 2018 .

Performance uncertainty propagation analysis for control-oriented model of a turbine-based combined cycle engine

Daren Yu, Juntao Chang, Jicheng Ma, 2018, Acta Astronautica.

Mathematical modeling and characteristic analysis for over-under turbine based combined cycle engine

Daren Yu, Wen Bao, Juntao Chang, 2018, Acta Astronautica.

Study on combustion mode transition of hydrogen fueled dual-mode scramjet engine based on thermodynamic cycle analysis

Juntao Chang, Zhongqi Wang, Jingfeng Tang, 2014 .

Flame oscillation characteristics in a kerosene fueled dual mode combustor equipped with thin strut flameholder

Chen Kong, Jun-tao Chang, Junlong Zhang, 2019, Acta Astronautica.

Ignition characteristics in a thin strut-equipped dual mode combustor fueled with liquid kerosene

Jun-tao Chang, Junlong Zhang, W. Bao, 2019, Acta Astronautica.

Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut

Jun-tao Chang, Junlong Zhang, W. Bao, 2019, Aerospace Science and Technology.

Research progress on strut-equipped supersonic combustors for scramjet application

Daren Yu, Junlong Zhang, Wen Bao, 2018, Progress in Aerospace Sciences.

Combustion stabilizations in a liquid kerosene fueled supersonic combustor equipped with an integrated pilot strut

Jun-tao Chang, Junlong Zhang, W. Bao, 2018, Aerospace Science and Technology.

Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut

Jun-tao Chang, Junlong Zhang, W. Bao, 2018 .

Research on flame prediction in a scramjet combustor using data-driven model

Ziao Wang, Chen Kong, Yunfei Li, 2022, Physics of Fluids.

Data-driven super-resolution reconstruction of supersonic flow field by convolutional neural networks

Ziao Wang, Chen Kong, Yunfei Li, 2021 .

Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators

Chen Kong, Jun-tao Chang, Yunfei Li, 2020 .

Flame Interaction Characteristics in Scramjet Combustor Equipped with Strut/Wall Combined Fuel Injectors

Jun-tao Chang, H. Tian, Junlong Zhang, 2020, Combustion Science and Technology.

Flame propagation and flashback characteristics in a kerosene fueled supersonic combustor equipped with strut/wall combined fuel injectors

Ziao Wang, Jun-tao Chang, Junlong Zhang, 2019, Aerospace Science and Technology.

Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine

Wen Bao, Juntao Chang, Lei Wang, 2014 .

Ignition Characteristics of a Liquid-Kerosene-Fueled Scramjet during Air Throttling Combined with a Gas Generator

Meng Wu, Daren Yu, Wen Bao, 2014 .

Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet

Juntao Chang, Wen Bao, Qingchun Yang, 2014 .

Research on combustion performance optimization in scramjet combustor with strut/wall combined fuel injection scheme

Jun-tao Chang, Junlong Zhang, W. Bao, 2021 .

Relative Time scale analysis for pressure propagation during ignition process of a scramjet

Wen Bao, Juntao Chang, Qingchun Yang, 2014 .

Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor

Jun-tao Chang, W. Bao, Chenlin Zhang, 2017 .

Dynamic Characteristics of Combustion Mode Transitions in a Strut-Based Scramjet Combustor Model

Wen Bao, Youhai Zong, Juntao Chang, 2013 .

Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine

Wen Bao, Juntao Chang, Qingchun Yang, 2015 .

A mechanism of combustion mode transition for hydrogen fueled scramjet

Jun Deng, Wen Bao, Juntao Chang, 2014 .

Analysis of combustion mode and operating route for hydrogen fueled scramjet engine

Daren Yu, Jiang Qin, Wen Bao, 2013 .

Oscillation of the shock train under synchronous variation of incoming Mach number and backpressure

Lianjie Yue, Wen-xin Hou, Yiming Li, 2022, The Physics of Fluids.

Hysteretic Behaviors of Separation-Shock Driven by Backpressure in Isolator with Incident Shocks

Nan Li, Jun-tao Chang, 2021 .

Oscillation of the shock train in an isolator with incident shocks

Wen Bao, Nan Li, Daren Yu, 2018, Physics of Fluids.

Prediction dynamic model of shock train with complex background waves

Daren Yu, Jun-tao Chang, Nan Li, 2017 .

Recent research progress on unstart mechanism, detection and control of hypersonic inlet

Nan Li, Daren Yu, Wen Bao, 2017 .

Hysteresis behavior of shock train driven by continuous incoming Mach number variation in an isolator with background waves

Chen Kong, Lianjie Yue, Ziao Wang, 2023, European Journal of Mechanics - B/Fluids.

Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence

Chen Kong, Yunfei Li, Chenlin Zhang, 2022, AIAA Journal.

Numerical Investigation on Performance of Axisymmetric Variable Geometry Scramjet Combustor Equipped with Strut Flame Holder

Junlong Zhang, W. Bao, Hongchao Qiu, 2021, Combustion Science and Technology.

Combustion characteristic using O2-pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet

Meng Wu, Daren Yu, Wen Bao, 2013 .

Mixing and combustion in supersonic/hypersonic flows

Li Yan, Wei Huang, Jun-tao Chang, 2020, Journal of Zhejiang University-SCIENCE A.

Flowing residence characteristics in a dual-mode scramjet combustor equipped with strut flame holder

Silong Zhang, Jun-tao Chang, Junlong Zhang, 2020 .

Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut

Junlong Zhang, Wen Bao, Juntao Chang, 2017 .

Study on influencing factors of combustion mode transition boundary for a scramjet engine based on one-dimensional model

Daren Yu, Yue Lu, R. Cao, 2020 .

Research on the operating boundary of the dual mode scramjet with a constant area combustor through thermodynamic cycle analysis

Jun-tao Chang, Junlong Zhang, W. Bao, 2020 .

Effect of continuous Mach number variation of incoming flow on ram–scram transition in a dual-mode combustor

Daren Yu, Junlong Zhang, Wen Bao, 2018 .

Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor

Wen Bao, Juntao Chang, Chenlin Zhang, 2017 .

A model of mode transition logic in dual-mode scramjet engines

Wen Bao, Juntao Chang, Xinyue Hao, 2016 .

Closed-loop control of shock train in inlet-isolator with incident shocks

Daren Yu, Juntao Chang, Nan Li, 2019, Experimental Thermal and Fluid Science.

Periodic forcing of a shock train in a scramjet inlet-isolator at overspeed condition

Daren Yu, Zhongqi Wang, X. Jiao, 2018 .

Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy

Daren Yu, Wen Bao, Juntao Chang, 2015 .

Recent progress of machine learning in flow modeling and active flow control

Jun-tao Chang, Yunfei Li, W. Bao, 2021, Chinese Journal of Aeronautics.

An efficient deep learning framework to reconstruct the flow field sequences of the supersonic cascade channel

Chen Kong, Yunfei Li, Ziao Wang, 2021 .

A deep learning approach for the velocity field prediction in a scramjet isolator

Ziao Wang, Chen Kong, Yunfei Li, 2021 .

Trajectory optimization for a TBCC-powered supersonic vehicle with transition thrust pinch

Daren Yu, Juntao Chang, Shengbo Yang, 2019, Aerospace Science and Technology.

Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor

Daren Yu, W. Bao, Chenlin Zhang, 2018 .

Experimental study on combustion mode transition effects in a strut-based scramjet combustor

Wen Bao, Jichao Hu, Youhai Zong, 2015 .

Experimental and numerical simulation of shock train characteristics in an isolator with incident shocks

Jialin Zheng, Yiming Li, Ziao Wang, 2023, Aerospace Science and Technology.

Experimental investigation of micro-ramp control for shock train under various incoming flow conditions

Chen Kong, Jun-tao Chang, Ziao Wang, 2022, Physical Review Fluids.

Experimental investigation of shock train behavior in a supersonic isolator

Daren Yu, Guangwei Wu, Ziao Wang, 2021 .

Instability of shock train behaviour with incident shocks

Daren Yu, Jun-tao Chang, Nan Li, 2020, Journal of Fluid Mechanics.

Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels

Chen Kong, Chengkun Lv, Ziao Wang, 2022, Acta Astronautica.

Path dependence characteristic of shock train in a 2D hypersonic inlet with variable background waves

Jun-tao Chang, W. Bao, Lin Gao, 2019, Aerospace Science and Technology.

Throttling process of a supersonic cascade studied by high-frequency response pressure and high-speed schlieren

Daren Yu, Ziao Wang, Wen-xin Hou, 2021, Scientific Reports.

Mechanism and detection of oscillatory flow in a supersonic cascade

Wen-xin Hou, Guangwei Wu, Ziao Wang, 2021 .

Shock train behavior affected by continuous Mach number variation of incoming flow

Ziao Wang, Jun-tao Chang, W. Bao, 2020 .

Propagation of shock-wave/boundary-layer interaction unsteadiness in attached and separated flows

Daren Yu, Ziao Wang, Jun-tao Chang, 2020 .

Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves

Daren Yu, Ziao Wang, Wen-xin Hou, 2020 .

Experimental investigation of mechanism and limits for shock train rapid forward movement

Daren Yu, Weixing Zhou, Juntao Chang, 2018, Experimental Thermal and Fluid Science.

Experimental study on the forced oscillation of shock train in an isolator with background waves

Chen Kong, Jun-tao Chang, W. Bao, 2020 .

Experimental study and analysis of shock train self-excited oscillation in an isolator with background waves

Chen Kong, Jun-tao Chang, W. Bao, 2020, Journal of Zhejiang University-SCIENCE A.

Behavior and flow mechanism of shock train self-excited oscillation influenced by background waves

W. Bao, Wen-xin Hou, Youyin Wang, 2020 .

Mathematical Model of Shock-Train Path with Complex Background Waves

Daren Yu, Wen Bao, Juntao Chang, 2017 .

Hysteresis phenomenon of hypersonic inlet at high Mach number

Daren Yu, Zhongqi Wang, Juntao Chang, 2016 .

Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement

Daren Yu, Weixing Zhou, Juntao Chang, 2016 .

Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions

Jun-tao Chang, B. Qin, Xiaoliang Jiao, 2015 .

A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor

Yingkun Li, W. Cai, Hui Sun, 2022, International Journal of Aerospace Engineering.

Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor

Wen Bao, Junlong Zhang, Juntao Chang, 2017 .

Combustion stabilization based on a center flame strut in a liquid kerosene fueled supersonic combustor

Jiang Qin, Wen Bao, Youhai Zong, 2013 .

Unstart/restart hysteresis characteristics analysis of an over–under TBCC inlet caused by backpressure and splitter

Nan Li, Daren Yu, Wen Bao, 2018 .

Flame Transition in Dual-Mode Scramjet Combustor with Oxygen Piloted Ignition

Wen Bao, Juntao Chang, W. Bao, 2014 .

Analysis of aerodynamic/propulsive couplings during mode transition of over-under turbine-based-combined-cycle engines

Daren Yu, Juntao Chang, Jialin Zheng, 2020 .

Coordinated control for regulation/protection mode-switching of ducted rockets

Jun Zhao, Wen Bao, Juntao Chang, 2014 .

Research on time sequence prediction of the flow field structure of supersonic cascade channels in wide range based on artificial neural network

Chen Kong, Yunfei Li, Weiyu Jiang, 2022, Physics of Fluids.

Scramjet Isolator Shock-Train Leading-Edge Position Modeling Based on Equilibrium Manifold

Jiang Qin, Wen Bao, Lei Wang, 2015 .

Short-term average wind speed and turbulent standard deviation forecasts based on one-dimensional convolutional neural network and the integrate method for probabilistic framework

Daren Yu, Jinfu Liu, Juntao Chang, 2020 .

Friction-Compensation Control of Gas-Flow Regulation for Ducted Rockets Based on Adaptive Dither Method

Bin Li, Daren Yu, Juntao Chang, 2013 .

Numerical investigation of the impact of asymmetric fuel injection on shock train characteristics

Daren Yu, Jun-tao Chang, B. Qin, 2014 .

Control-oriented unsteady one-dimensional model for a hydrocarbon regeneratively-cooled scramjet engine

Daren Yu, Junlong Zhang, Wen Bao, 2019, Aerospace Science and Technology.

Recent research progress on airbreathing aero-engine control algorithm

Jun-tao Chang, W. Bao, D. Yu, 2022, Propulsion and Power Research.

Multivariable control of regeneratively-cooled scramjet engine with two-stage kerosene injection based on H∞ method

Daren Yu, Hao Liu, Juntao Chang, 2020 .

Multi-objective coordinated control of regeneratively-cooled scramjet engine with two-stage kerosene injection

Daren Yu, Wen Bao, Juntao Chang, 2019, Aerospace Science and Technology.

Control-oriented modeling and real-time simulation method for a dual-mode scramjet combustor

Daren Yu, Junlong Zhang, Juntao Chang, 2018, Acta Astronautica.

Indirect measurement method of inner wall temperature of scramjet with a state observer

Jiang Qin, Wen Bao, Cong Zhang, 2015 .

Thermodynamic modeling and analysis of ammonia injection pre-compressor cooling cycle: A novel scheme for high Mach number turbine engines

Jun-tao Chang, D. Yu, Fuxu Quan, 2022, Energy Conversion and Management.

Richtmyer-Meshkov Instability Induced Mixing Enhancement in the Scramjet Combustor with a Central Strut

Qingchun Yang, Jun-tao Chang, W. Bao, 2014 .

Noise-Suppressed Temperature Measurement Based on Machine Learning in a Scramjet Combustor

Junlong Zhang, W. Bao, Jun-tao Chang, 2021 .

Prediction model of temperature field in dual-mode combustors based on wall pressure

Chen Kong, Yunfei Li, Jingfeng Tang, 2022, Acta Astronautica.

Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel

Daren Yu, Juntao Chang, Zhongqi Wang, 2017 .

Effects of Air Vitiation on Scramjet Performance Based on Thermodynamic Cycle Analysis

Junlong Zhang, Wen Bao, Juntao Chang, 2014 .

Flow field reconstruction and prediction of the supersonic cascade channel based on a symmetry neural network under complex and variable conditions

Juntao Chang, Ziao Wang, Yunfei Li, 2020, AIP Advances.

Investigations on flowfield behavior and resistance backpressure characteristics of supersonic cascade with boundary layer suction

Ziao Wang, Jun-tao Chang, Junlong Zhang, 2018, Acta Astronautica.

Prediction model of flow field in an isolator over various operating conditions

Ziao Wang, Chen Kong, Juntao Chang, 2021 .

Thrust control system design of ducted rockets

Bin Li, Daren Yu, Juntao Chang, 2011 .

Operation pattern classification of hypersonic inlets

Daren Yu, Yi Fan, Wen Bao, 2009 .

Optimal Classification Criterions of Hypersonic Inlet Start/Unstart

Daren Yu, Wen Bao, Juntao Chang, 2007 .

Nonlinear characteristics and detection of combustion modes for a hydrocarbon fueled scramjet

Wen Bao, Juntao Chang, Qingchun Yang, 2015 .

Novel Oscillatory Patterns of Hypersonic Inlet Buzz

J. Qin, Jun-tao Chang, W. Bao, 2012 .

A Bayesian data assimilation method to enhance the time sequence prediction ability of data-driven models

Chen Kong, Jun-tao Chang, Yunfei Li, 2022, AIP Advances.

Robust asynchronous bumpless transfer for switched linear systems

Wen Bao, Juntao Chang, Yiwen Qi, 2015, Int. J. Control.

Short-term probabilistic predictions of wind multi-parameter based on one-dimensional convolutional neural network with attention mechanism and multivariate copula distribution estimation

Jinfu Liu, Daren Yu, Mingliang Bai, 2021 .

Effect of structural factors on maximum aerodynamic heat flux of strut leading surface

Daren Yu, Jun-tao Chang, W. Bao, 2014 .

Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection

Wen Bao, Juntao Chang, John Z. Wen, 2014 .

Investigation of shock wave control by suction in a supersonic cascade

Ziao Wang, Chen Kong, Jun-tao Chang, 2021 .

Switching control of thrust regulation and inlet buzz protection for ducted rocket

Bin Li, Daren Yu, Juntao Chang, 2010 .

Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor

Daren Yu, Wen Bao, Juntao Chang, 2018, Aerospace Science and Technology.

Effect of heat release on movement characteristics of shock train in an isolator

Wen Bao, Juntao Chang, Wen Shi, 2017 .

Supersonic Inlet Dynamics Model Based on Equilibrium Manifold

Daren Yu, Jun-tao Chang, W. Bao, 2006 .

Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust

Wen Bao, Juntao Chang, Jun-tao Chang, 2014, TheScientificWorldJournal.

Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl

Junlong Zhang, W. Bao, Wen-xin Hou, 2018, Acta Astronautica.

Backpressure unstart detection for a scramjet inlet based on information fusion

Daren Yu, Wen Bao, Lei Wang, 2014 .

Unstart margin control of hypersonic inlets

Daren Yu, Wen Bao, Yi Shen, 2010 .