Open Access
| Issue |
JNWPU
Volume 36, Number 6, December 2018
|
|
|---|---|---|
| Page(s) | 1193 - 1201 | |
| DOI | https://doi.org/10.1051/jnwpu/20183661193 | |
| Published online | 12 March 2019 | |
- Baudart P, Duthoit V, Harlay J. Numerical Simulation of Cryotechnic Rocket Engine Ignition[C]//Joint Propulsion Conference, 2013 [Google Scholar]
- Buttay R, Gomet L, Lehnasch G, et al. Highly Resolved Numerical Simulation of Combustion Downstream of a Rocket Engine Igniter[J]. Shock Waves, 2017, 27(4): 1-20 [Article] [CrossRef] [Google Scholar]
- Popp M, Stanke J. Experimental Investigation of the HM7B Thrust Chamber Start-Up Transient[C]//Joint Propulsion Conference, 2013 [Google Scholar]
- Cho Yongho, Chang Haengsoo. Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG[C]//AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2013 [Google Scholar]
- Agostino L D, Biagioni L, Lamberti G. An Ignition Transient Model for Solid Propellant Rocket Motors[C]//Joint Propulsion Conference & Exhibit, 2001 [Google Scholar]
- William A D, Michael T H, Robert Fiedler. Integrated 3-D Simulation of Solid Propellant Rockets[C]//Joint Propulsion Conference & Exhibit, 2001 [Google Scholar]
- Fielder R A, Breitenfeld M S, Jiao X, et al. Simulations of Slumping Propellant and Flexing Inhibitors in Solid Rocket Motors[C]//Joint Propulsion Conference & Exhibit, 2002 [Google Scholar]
- Fielder R, Jiao X, Namazifard A, et al. Coupled Fluid-Structure 3-D Solid Rocket Motor Simulation[C]//Joint Propulsion Conference & Exhibit, 2001 [Google Scholar]
- Chen Bo, Lin Mu, Wu Baoyuan, et al. Numerical Study on Igniter Performance of Liquid Ramjet Combustor[J]. Journal of Rocket Propulsion, 2013, 39(6): 6-11 (in Chinese) [Article] [NASA ADS] [Google Scholar]
- Li Chunhong, Zhang Xiaoping, Ma Dongying, et al. Ignition Scheme of LOX/Methane Gas Generator[J]. Journal of Rocket Propulsion, 2010, 36(5): 7-12 (in Chinese) [Article] [Google Scholar]
- Wu Hongbin. Pyrotechnic Igniters and Electrical Spark Igniters for LOX/LH2 Rocket Engines[J]. Missiles and Space Vehicles, 1994, 211(5): 32-42 (in Chinese) [Article] [Google Scholar]
- Yang Le, Yu Zhenyong, He Jingxuan. A Fluent Analysis of Influencing Factors for SRM Inner Flow Field Simulation at Ignition[J]. Journal of Solid Rocket Technology, 2011, 34(4): 474-477 (in Chinese) [Article] [Google Scholar]
- Yang Le, Yu Zhenyong, He Jingxuan. Calculation Model of Inner Flow Field of Solid Rocket Motor in Ignition Transient[J]. Missiles and Space Vehicles, 2015(6); 75-77 (in Chinese) [Article] [Google Scholar]
- Tang Bishun, Chen Jun, Feng Feng, et al. Numerical Simulation of Diaphragm Rupture Process of Igniter in Ignition Process of Solid Rocket Motor[J]. Journal of Solid Rocket Technology, 2013, 36(6): 753-757 (in Chinese) [Article] [Google Scholar]
- Xu Xuewen, Mu Junlin Ren Jiancun et al. The Analyses of Transient Flow-Field Characteristics in Nozzle of SRM Journal of Rocket Propulsion 2015 41(5): 49-53 (in Chinese) [Article] [Google Scholar]
- Wu Xiong, Zhang Weihua. Simulation of the Flowfield in Secondary Injection Vector Control Nozzle for Solid Rocket Motor[J]. Journal of National University of Defense Technology, 2006(2): 22-25 (in Chinese) [Article] [Google Scholar]
- Lin Qingguo, Zhou Jin. A Numerical Study of Combustion and Heat Transfer in Small Thrust Liquid Rocket Engine[J]. Journal of National University of Defense Technology, 2012, 34(4): 13-17 (in Chinese) [Article] [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.