近年来发表文章(*为通讯作者)
1.Qi-fan Zhang, Hui-jun Tan, Hao Chen, Yong-qin Yuan and Yu-chao Zhang. Unstart Process of a Rectangular Hypersonic Inlet at Different Speeds, AIAA Journal, Vol. 54, No. 12, pp. 3681-3691, 2016.
2.Qi-fan Zhang, Hui-jun Tan, Shu Sun, Huan-xian Bu and Cai-yan Rao. Unstart of a Hypersonic Inlet with Side Compression Caused by Downstream Choking, AIAA Journal, Vol. 54, No. 1, pp. 28-38, 2016.
3.张启帆,岳连捷,贾轶楠,张新宇,等. 真实气体效应对Ma10级进气道流动的影响.推进技术,2019, 40(5): 1042-1050.
4.贾轶楠,张启帆*,仝晓通,岳连捷,张新宇. 内压缩波系对高超声速进气道自起动性能影响研究. 实验流体力学, 2019, 33(3): 60-67.
5.张启帆, 谭慧俊, 陈昊. 基于滑动多缝板的高超声速进气道不起动振荡流态控制实验研究,推进技术, 2017, 38(7): 1450-1458.
6.张旭,吴振杰,张启帆*,等. 超声速燃烧迟滞双环试验研究.第十二届全国高超声速科技学术会议,绵阳,2019.(会议优秀论文)
7.仝晓通,张启帆*,等. 引压管结构对动态压力测量结果的影响. 第一届发动机内流气动技术交流会,西宁,2018.(会议优秀论文)
8.Xu zhang, Lianjie Yue, Tinglong Huang, Qifan Zhang, Xinyu Zhang. Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor. Aerospace Science and Technology 2019, 94:105420.
9.Hao Chen, Huijun Tan, Yazhou Liu, and Qifan Zhang. External compression supersonic inlet free from violent buzz. AIAA Journal 2019, 57(6): 2513-2523.
10.王晨曦,谭慧俊,张启帆,孙姝. 高超声速进气道低马赫数不起动和再起动试验, 航空学报, 2017, 38(11):121146.
发明专利:
一种进气道定堵塞度自起动试验装置,授权号ZL201710941567.2,第一完成人。