Numerical and experimental researches for the high-speed flows

04/2012 - Now:    Institute of Mechanics, Postdoc Researcher, Assistant Professor, Associate Professor, and Professor
10/2008 - 3/2012: Nagoya University, Japan. PhD Degree 

   

1.     Yue Wang; Yunpeng Wang*; Chun Wang; Zonglin Jiang, Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle,                
Journal of Spacecraft and Rockets (AIAA Journal), 2023, 60(1):215-229.
2.     Yue Wang; Yunpeng Wang*; Zonglin Jiang, Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel, AIAA Journal, 2022, 60(12):6940-6946. 
3.     Yunpeng Wang*; Zonglin Jiang, Theories and Methods for Designing Hypersonic High-Enthalpy Flow Nozzles, Chinese Journal of Aeronautics, 2022, 35(1):318–339.
4.     汪运鹏*; 杨瑞鑫; 聂少军; 姜宗林, 基于深度学习技术的激波风洞智能测力系统研究, 力学学报, 2020, 52(5):1304-1313.
5.     Yunpeng Wang*; Zonglin Jiang, Impulse force-measurement system, Shock Waves, 2020, 30(6):1–11.
6.     Yunpeng Wang*; Zonglin Jiang; et al., Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel., Shock waves, 2016, 26(6):835-844.
7.     Yunpeng Wang*; Yunfeng Liu; Changtong Luo; Zonglin Jiang, Force measurement using strain-gauge balance in a shock tunnel with long test duration, Review of Scientific Instruments, 2016, 87, 055108.
8.     Yunpeng Wang*; Zongmin Hu; Yunfeng Liu; Zonglin Jiang, Starting Process in a Large-Scale Shock Tunnel, AIAA Journal, 2016, 54(4):1240-1249.
9.     Yunpeng Wang*; Hiroshi Ozawa; Hiroto Koyama; Yoshiaki Nakamura, Abort Separation of Launch Escape System Using Aerodynamic Interference, AIAA Journal, 2013, 51(1):270-275.
10.   汪運鵬*; 田中潤治; 轟木峻; 土井克則; 中村佳朗, 表面移動法によるフラップ表面の剥離流制御, 日本航空宇宙学会論文集, 2010, 58:239-244.

Other publications: ResearchGate

High-temperature gasdynamics, CFD, Aerodynamic measurements in wind tunnel.

• Development of Strain Gauge Balance for the JF12 Shock Tunnel, 10st International Symposium on Strain-Gaged Balances, Mianyang, China, May 13-19, 2016.

• Aerodynamic Force and Moment Measurement under Duplicated Hypersonic Flight Conditions in the JF12 Shock Tunnel, 30th International Symposium of Shock Waves, Tel-Aviv, Israel, July 19-24, 2015.

• Numerical Investigation of the Starting Process in a Long-Test-Duration Hypervelocity Shock Tunnel, 22th AIAA Computational Fluid Dynamics Conference, Dallas, Texas, USA, Jun. 22-26, 2015, AIAA Paper 2015-2291.

• Force Measurement Using A Pulse-type Strain-Gaged Balance in Hypersonic Shock Tunnel, the proceedings of the 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, March 2-6, 2015.

• Study and Analyses on the Structural Performance of Strain-Gaged Balance for a Long-Test Duration Shock Tunnel, 9th International Symposium on Strain-Gaged Balances, Seattle, Washington, USA, May 19-22, 2014.

• Force Measurement of Cones Using High-Stiffness Strain-Gauge Balance in Long-Test Duration Shock Tunnel, 1st International High-Speed Flow Conference, Beijing, China, May 13-14, 2014.

• Simulation of Supersonic Stage Separation of Capsule-Shaped Abort System by Aerodynamic Interaction, 20th AIAA Computational Fluid Dynamics Conference, Honolulu, Hawaii, USA, Jun. 2011, AIAA Paper 2011-3064.

• Numerical Simulation of Emergency Separation for Capsule Abort System Using Supersonic Aerodynamic Interaction between Two Bodies, 24th Symposium on Computational Fluid Dynamics, F11-3, Yokohama, Japan, Dec 2010.