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Dengke Li, Bo Sun*, Chunliang Dai, Xiong Chen, Xiang Zhang, Yanjin Man. Influences of thermochemical non-equilibrium effects on Type III shock/shock interaction at Mach 10. Acta Astronautica, 214 (2024) 553–566.
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王奕凯, 孙波*, 李登科, 等. 基于Zukauskas关系式的预冷发动机进气道流动特性研究[J]. 推进技术. 2024, 45（1）：2208079.
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Chunliang Dai, Bo Sun, Dan Zhao, Weixuan Li, Xiran Liu, Yue Zhang, Hexia Huang, Xu Dong. Mode identification and decomposition analysis of self-excited thermodynamic oscillations in hypersonic inlet/isolator of a scramjet. Aerospace Science and Technology, 144 (2024) :108820.
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Chunliang Dai , Bo Sun*, Dan Zhao, Shengbing Zhou, Changsheng Zhou, Yanjin Man High temperature non-equilibrium flow characteristics of impinging shock/flat-plate turbulent boundary layer interaction at Mach 8.42 [J]. Physics of Fluids, 2023, 35, 095128.
Chunliang DAI, Bo SUN*, Lianjie YUE, Shengbing ZHOU, Changfei ZHUO, Changsheng ZHOU, Jianyi YU. Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range [J]. Chinese Journal of Aeronautics, 2023.
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代春良，孙波，卓长飞，等. 前缘钝化和化学非平衡效应对斜爆震发动机进气道特性的影响［J］. 推进技术，2022，43（1）：200751.
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Chunliang Dai, Bo Sun*, Changfei Zhuo, et al. Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow. AerospaceScienceandTechnology124, 2022, 107526.
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XIA Feng，SUN Bo*，YU Jianyi, et al. Flow and leakage characteristics in sealing chamber of a variable geometry hypersonic inlet［J］. Transactions of Nanjing University of Aeronautics and Astronautics，2022,39(6)：663?671.
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Chunliang Dai, Bo Sun∗, Shengbing Zhou, et al . Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet. Acta Astronautica 193 (2022) 237–254.
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丁宋毅，孙波，卓长飞，等. 高超声速进气道内粉末燃料喷注及流动控制特性研究［J］. 推进技术，2022，43（12）：210489.
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Chunliang Dai, Bo Sun∗, Changsheng Zhou, et al . Numerical investigation of real-gas effect of inward-turning inlet at Mach12. Aerospace Science and Technology,115 (2021):106786.
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孙波,卓长飞. 内流激波边界层干扰非对称特性研究综述[J]. 气动研究与实验, 2021, 33(04): 15-22.
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王海，孙波*，卓长飞，满延进，李宏东. 预冷发动机进气道节流特性数值研究. 航空动力学报. 2021,36(03).
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杜磊，孙波*，代春良，卓长飞. 壁面温度对斜爆震发动机进气道流动特性影响的数值研究. 推进技术. 2021,42(04).
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代春良，孙波，梁晓扬，卓长飞，张堃元．真实气体效应下高马赫数内转进气道特性研究．推进技术,2020.
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Sun, B.; Wang, C.; Zhuo, C. Theoretical Model and Numerical Analysis for Asymmetry of Shock Train in Supersonic Flows. Symmetry 2020, 12, 518. SCIE
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SUN Bo，XIANG Cuiling，ZHUO Changfei. Back Pressure Characteristics for Turbine Channel of External?Parallel TBCC Inlet. Transactions of Nanjing University of Aeronautics and Astronautics，2019，36（5）：808?816.
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代春良，孙波*，张堃元．马赫数３～６宽速域内转进气道优化设计．航空动力学报，2019, 34(10).
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闵浩，孙波，李嘉新，邬凤林，张堃元.一种内并联型内转进气道通道间干扰特性研究.推进技术，2018,39(12).
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Xiaoqian Chen, Bo Sun*, Chunliang Dai, and Xiangang Wang. Wind energy harvesting using jet-edge flow oscillations. AIP Advances,2018,8, 095018.SCI
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Luo Xiaochen, Sun Bo*, Wang Xiang'ang. Experimental investigation on a cavity-step-actuated supersonic oscillating jet. Chinese Journal of Aeronautics, 2017, 30(1): 274–281.SCI
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孙波,邵庆龄,倪凯捷,卓长飞,张堃元.并联TBCC可调进气道并联方案.航空动力学报，2017,32（12）.EI
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Bo Sun, Feng Feng, Xiao-song Wu, Xiao-chen Luo*. Experimental Investigations of Cavity-actuated Supersonic Oscillating Jet. Experimental Thermal and Fluid Science，2015, 68: 155-162.( SCIE: 000365361800015, JCR：3区，IF：1.99)
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Bo Sun, Xiao-chen Luo*,Feng Feng, Xiao-song Wu. Experimental investigation on cavity-actuated under-expanded supersonic oscillating jet, 2015, 28(5): 1372–1380.( SCIE: 000367071000007,JCR：4区，IF：1.07)