共 20 条
- [1] WANG Chen, WANG Xiaojun, ZHANG Hongjian, Et al., Research on the development of reusable launch vehicle, Aerodynamic Missile Journal, 9, (2018)
- [2] GAO Zhaohui, ZHANG Puzhuo, LIU Yu, Et al., Analysis of vertical landing technique in reusable launch vehicle, Journal of Astronautics, 37, 2, (2016)
- [3] WANG Xiaowei, ZHANG Puzhuo, WU Shengbao, Et al., Recovery technology of launch vehicle stage, Spacecraft Recovery & Remote Sensing, 37, 3, (2016)
- [4] KLEVANSKI J, ECKER T, RIEHMER J, Et al., Aerodynamic studies in preparation for callisto-Reusable VTVL launcher first stage demonstrator, Proceedings of the 69th International Astronautical Congress, (2018)
- [5] ZILKER F., Aerothermal analysis of re-usable first stage during rocket retro-propulsion, (2018)
- [6] RINCON M j., Supersonic retropopulsion CFD analysis of a reusable vertical landing rocket, (2018)
- [7] ECKER T, KARL S, DUMONT E, Et al., A numerical study on the thermal loads during a supersonic rocket retro-propulsion maneuver, Proceedings of the 53rd AIAA/SAE/ASEE Joint Propulsion Conference, (2017)
- [8] WANG Zejiang, LI Jie, ZENG Xuejun, Et al., Effect of opposing jet on drag reduction characteristics of double-cone missile shape, Acta Aeronautica et Astronautica Sinica, 41, 12, (2020)
- [9] LEE J, LEE H J, HUH H., Drag reduction analysis of counterflow jets in a short penetration mode, Aerospace Science and Technology, 106, (2020)
- [10] EGHLIMA Z, MANSOUR K, FARDIPOUR K., Heat transfer reduction using combination of spike and counterflow jet on blunt body at high Mach number flow, Acta Astronautica, 143, (2018)