共 50 条
- [21] Effects of the nozzle throat diameter on the flow properties of an inductively coupled plasma heaterJOURNAL OF THE KOREAN PHYSICAL SOCIETY, 2021, 79 (11) : 1019 - 1026Yu, MinghaoWang, Zhe
- [22] A fluidic thrust vector control using the bypass flow in a dual throat nozzleJournal of Mechanical Science and Technology, 2021, 35 : 3435 - 3443Kexin WuHeuyDong Kim
- [23] Effects of the nozzle throat diameter on the flow properties of an inductively coupled plasma heaterJournal of the Korean Physical Society, 2021, 79 : 1019 - 1026Minghao YuZhe Wang
- [24] A fluidic thrust vector control using the bypass flow in a dual throat nozzleJOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2021, 35 (08) : 3435 - 3443Wu, KexinKim, HeuyDong
- [25] Vibrationally Relaxing Gas Flow in a Nozzle with a Constant Cross Section at the Throat.1984,Sal'nikov, V.A.
- [26] Effects of downstream throat on aerodynamic performance of dual throat nozzleHangkong Dongli Xuebao, 3 (580-587):Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing210016, China
- [27] Numerical Study on the Effect of the Nozzle Pressure Ratio on the Starting Characteristics of the Axisymmetric Divergent Dual Throat NozzleFLUID DYNAMICS, 2024, 59 (03) : 612 - 621Wang, Y. S.Xu, J. L.Huang, S.
- [29] Rocket nozzle throat technology advancesAVIATION WEEK & SPACE TECHNOLOGY, 2003, 158 (24): : 199 - 199Rosenberg, B
- [30] ELECTROFORMING OF A THROAT NOZZLE FOR A COMBUSTION FACILITYPLATING AND SURFACE FINISHING, 1977, 64 (08): : 44 - 51DINI, JWJOHNSON, HR