| Recent research progress on unstart mechanism, detection and control of hypersonic inlet J Chang, N Li, K Xu, W Bao, D Yu Progress in Aerospace Sciences 89, 1-22, 2017 | 214 | 2017 |
| Research progress on strut-equipped supersonic combustors for scramjet application J Chang, J Zhang, W Bao, D Yu Progress in Aerospace Sciences 103, 1-30, 2018 | 164 | 2018 |
| One-day-ahead probabilistic wind speed forecast based on optimized numerical weather prediction data X Zhao, J Liu, D Yu, J Chang Energy Conversion and Management 164, 560-569, 2018 | 114 | 2018 |
| Switching control of thrust regulation and inlet buzz protection for ducted rocket W Bao, B Li, J Chang, W Niu, D Yu Acta Astronautica 67 (7-8), 764-773, 2010 | 84 | 2010 |
| Oscillation of the shock train in an isolator with incident shocks N Li, JT Chang, KJ Xu, DR Yu, W Bao, YP Song Physics of Fluids 30 (11), 2018 | 82 | 2018 |
| Prediction dynamic model of shock train with complex background waves N Li, JT Chang, KJ Xu, DR Yu, W Bao, YP Song Physics of Fluids 29 (11), 2017 | 82 | 2017 |
| Dynamic characteristics of combustion mode transitions in a strut-based scramjet combustor model W Bao, Q Yang, J Chang, Y Zong, J Hu Journal of Propulsion and Power 29 (5), 1244-1248, 2013 | 79 | 2013 |
| Novel oscillatory patterns of hypersonic inlet buzz J Chang, L Wang, W Bao, J Qin, J Niu, W Xue Journal of Propulsion and Power 28 (6), 1214-1221, 2012 | 77 | 2012 |
| Short-term average wind speed and turbulent standard deviation forecasts based on one-dimensional convolutional neural network and the integrate method for probabilistic framework X Zhao, N Jiang, J Liu, D Yu, J Chang Energy Conversion and Management 203, 112239, 2020 | 76 | 2020 |
| Mechanism and prediction for occurrence of shock-train sharp forward movement K Xu, J Chang, W Zhou, D Yu AIAA Journal 54 (4), 1403-1412, 2016 | 74 | 2016 |
| A deep learning approach for the velocity field prediction in a scramjet isolator C Kong, J Chang, Y Li, Z Wang Physics of Fluids 33 (2), 2021 | 65 | 2021 |
| Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut J Zhang, J Chang, J Ma, C Zhang, W Bao Aerospace Science and Technology 70, 152-160, 2017 | 65 | 2017 |
| Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut J Zhang, J Chang, J Ma, Y Wang, W Bao Aerospace Science and Technology 84, 686-697, 2019 | 63 | 2019 |
| Optimal classification criterions of hypersonic inlet start/unstart D Yu, J Chang, W Bao, Z Xie Journal of Propulsion and Power 23 (2), 310-316, 2007 | 62 | 2007 |
| Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves Z Wang, J Chang, W Hou, D Yu Physics of Fluids 32 (5), 2020 | 61 | 2020 |
| Analysis of combustion mode and operating route for hydrogen fueled scramjet engine R Cao, J Chang, W Bao, M Guo, J Qin, D Yu, Z Wang International journal of hydrogen energy 38 (14), 5928-5935, 2013 | 57 | 2013 |
| Unstart/restart hysteresis characteristics analysis of an over–under TBCC inlet caused by backpressure and splitter N Li, J Chang, C Jiang, D Yu, W Bao, Y Song, X Jiao Aerospace Science and Technology 72, 418-425, 2018 | 52 | 2018 |
| Flowfield reconstruction and shock train leading edge detection in scramjet isolators C Kong, J Chang, Y Li, N Li AIAA Journal 58 (9), 4068-4080, 2020 | 50 | 2020 |
| Mechanism study on local unstart of hypersonic inlet at high Mach number X Jiao, J Chang, Z Wang, D Yu AIAA Journal 53 (10), 3102-3112, 2015 | 50 | 2015 |
| Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection J Hu, J Chang, W Bao, Q Yang, J Wen Acta Astronautica 104 (1), 84-90, 2014 | 50 | 2014 |
