[23]

Jiarui Wei, Yu Shen, Fengyuan Zuo*. XXXXXXX. To be submit.

[22]

Fengyuan Zuo*. Hypersonic conical shock wave/turbulent boundary layer interaction at high Reynolds number. AIAA Journal. Accept.

[21]

Fengyuan Zuo*, Antonio Memmolo, Sergio Pirozzoli*. On wall pressure fluctuations in conical shock wave/turbulent boundary layer interaction. Journal of Fluid Mechanics. Minor Revision.

[20]

Fengyuan Zuo*, Sannu Mölder. Design of hypersonic wavecatcher intake at Mach 12 with rectangular-to-elliptical shape transition. Propulsion and Power Research. Accept.

[19]

Fengyuan Zuo*. Hypersonic shock wave/turbulent boundary layer interaction over a compression ramp. AIAA Journal. 2023, 61(4): 1579-1595.

[18]

Fengyuan Zuo*, Ming Yu, Sergio Pirozzoli. Modal analysis of separation bubble unsteadiness in conical shock-wave/turbulent-boundary-layer interaction. AIAA Journal. 2022, 60(9): 5123-5135.

[17]

Fengyuan Zuo*, Jiarui Wei, Shuling Hu, Sergio Pirozzoli. Effects of wall temperature on hypersonic impinging shock wave/turbulent boundary layer interactions. AIAA Journal. 2022, 60(9): 5109-5122.

[16]

Fengyuan Zuo*, Sannu Mölder. Startability of truncated hypersonic wavecatcher intake. Acta Astronautica. 2022, 198: 531-540.

[15]

Fengyuan Zuo*, Sannu Mölder, Shuling Hu. Thermochemical non-equilibrium effects on hypersonic wavecatcher intake at Mach 12. Acta Astronautica. 2022, 198: 56-68.

[14]

Fengyuan Zuo*, Sannu Mölder. Flow quality in an M-Busemann wavecatcher intake. Aerospace Science and Technology. 2022, 121: 107376.

[13]

Fengyuan Zuo*, Antonio Memmolo, Sergio Pirozzoli. Reynolds-averaged numerical simulations of conical shock wave/boundary layer interactions. AIAA Journal. 2021, 59(5): 1645-1659.

[12]

Fengyuan Zuo*. The scaling of separation bubble in the conical shock wave/turbulent boundary layer interaction. Acta Astronautica. 2021, 186: 418-425.

[11]

Fengyuan Zuo*, Shuling Hu. Thermochemical non-equilibrium effects on aerothermodynamic prediction of laminar double-cone flow. Acta Astronautica. 2021, 182: 179-188.

[10]

Fengyuan Zuo*, Sannu Mölder, Gang Chen. Performance of wavecatcher intakes at angles of attack and sideslip. Chinese Journal of Aeronautics. 2021, 34(7): 244-256. (Editor’s Highlights)

[9]

Fengyuan Zuo*, Antonio Memmolo. Investigation of conical shock wave/boundary layer interaction in axisymmetric internal flow. Aerospace Science and Technology. 2020, 106: 106106.

[8]

Fengyuan Zuo*, Antonio Memmolo, Guoping Huang, Sergio Pirozzoli*. Direct numerical simulation of conical shock wave-turbulent boundary layer interaction. Journal of Fluid Mechanics. 2019, 877: 167-195. (Featured on cover)

[7]

Fengyuan Zuo*, Sannu Mölder. Hypersonic wavecatcher intakes and variable-geometry turbine based combined cycle engines. Progress in Aerospace Sciences. 2019, 106: 108-144. (Invited Review)

[6]

Fengyuan Zuo*, Guoping Huang. Numerical investigation of bleeding control method on section-controllable wavecatcher intakes. Acta Astronautica. 2018, 151: 572-584.

[5]

Fengyuan Zuo*, Guoping Huang, Chen Xia. Investigation of internal-waverider-inlet flow pattern integrated with variable-geometry for TBCC. Aerospace Science and Technology. 2016, 59: 69-77.

[4]

Fengyuan Zuo*, Guoping Huang, Chen Xia. Bleeding control for improving internal waverider inlet self-starting ability. International Journal of Turbo & Jet-Engines. 2019, 36(1): 51-60.

[3]

Guoping Huang, Fengyuan Zuo*, Wenyou Qiao. Design method of internal waverider inlet under non-uniform upstream for inlet/forebody integration. Aerospace Science and Technology. 2018, 74: 160-172.

[2]

左逢源*. 内转式TBCC组合动力进气道设计方法研究进展. 清华大学学报(自然科学版), 2022, 62 (3): 555-561. 

[1]

左逢源, et.al. 基于内乘波概念的TBCC进气道过渡模态研究. 工程热物理学报, 2015, 36(02): 274-278. 

[7]

左逢源, 第二届空气动力学会议，天津，2023.4 

[6]

左逢源, 第二十届全国激波与激波管会议,  中科大,  合肥, 2022.7 (分会场邀请报告)

[5]

左逢源,  第十二届全国流体力学会议,  2022.11

[4]

左逢源,  中国力学大会-2021,  2022.11

[3]

Fengyuan Zuo*, Guoping Huang, Chen Xia, Weiyuan Tang. Investigation of the self-starting ability of an internal waverider inlet for ramjet. 51st AIAA Joint Propulsion Conference. Orlando, FL, United states: AIAA Paper 2015-3748, 2015.

[2]

Fengyuan Zuo*, Guoping Huang, Huihui Huang, Chen Xia. Analyzing the parent flowfield of inward turning inlet combined with variable-geometry. 52nd AIAA Joint Propulsion Conference. Salt Lake City, UT, United states: AIAA Paper 2016-4574, 2016. 

[1]

Fengyuan Zuo*, Guoping Huang. A preliminary overview analysis on the internal waverider inlets for ramjet. 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China: AIAA Paper 2017-2420, 2017.