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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)
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南向军,张堃元*,金志光,孙波. 矩形转圆形高超声速内收缩进气道数值及实验研究.航空学报,第32卷,第6期,988-996页, 2011. (EI: 20112814137367)
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南向军, 张堃元*, 金志光, 孙波. 压升规律可控的高超声速内收缩进气道设计. 航空动力学报,第26卷,第3期,518-523页,2011. (EI: 20112013987438)
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Sun B, Zhang K Y*. Empirical Equation for Self-Starting Limit of Supersonic Inlets. Journal of Propulsion and Power, Vol. 26, No.4, pp. 874-875, 2010. (SCI: 000280255300028)
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Sun B, Zhang K Y*, Wang C P, and Wu X S. Investigation on a Streamtraced Hypersonic Busemann Inlet. Proc. IMechE, Part G: J. Aerospace Engineering, Vol. 224, No. G1, pp.57-63, 2010. (SCIE: 000273895700005)
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孙波,张堃元,武晓松. 弹用模块化Busemann进气道数值研究[J]. 航空动力学报, 2009,24(3):573-580. (EI: 20091612036304)