Open Access
Issue |
JNWPU
Volume 38, Number 1, February 2020
|
|
---|---|---|
Page(s) | 170 - 175 | |
DOI | https://doi.org/10.1051/jnwpu/20203810170 | |
Published online | 12 May 2020 |
- Luo Jinling. Inspiration of Hypersonic Vehicle with Airframe/Propulsion Integrated Design[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 39–48 [Article] (in Chinese) [Google Scholar]
- Tan Huijun, Bu Huanxian, Zhang Qifan, et al. Review of Hypersonic Inlet Unstart Phenomenon[J]. Journal of Nanjing University of Aeronautics&Astronautics, 2014, 46(4): 501–508 [Article] (in Chinese) [Google Scholar]
- Li Liugang, Tan Huijun, Sun Shu, et al. Signal Characteristics and Prediction of Unstarting Process for Two-Dimensional Hypersonic Inlet[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(12): 2324–2331 [Article] (in Chinese) [Google Scholar]
- Wang Chenxi, Tan Huijun, Zhang Qifan, et al. Test of Low Mach Number Unstart and Restart Process of Hypersonic Inlet[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(11):121146 [Article] (in Chinese) [Google Scholar]
- Guo Shuaitao, Li Zhufei, Gao Wenzhi, et al. Analogy between Effects of Attack Angle and Mach Number on Inlet Starting[J]. Journal of Propusion Technology, 2017, 38(5): 983–991(in Chinese) [Google Scholar]
- Hutchins E, Akella R, Clemens T. Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart[C]//AIAA Flow Control Conference, 2012 [Google Scholar]
- Pettinari S, Corradini M L, Serrani A. Detection of Scramjet Unstart in a Hypersonic Vehicle Model[C]//American Control Conference, 2012 [Google Scholar]
- Shadab M A, Baig M F. Investigation and Control of Unstart Phenomenon in Scramjets[C]//AIAA International Space Planes and Hypersonic System and Technologies Conference, 2017 [Google Scholar]
- Bolender M A, Wilkin H, Jacobsen L, et al. Flight Dynamics of a Hypersonic Vehicle during Inlet Un-Start[C]//AIAA International Space Planes and Hypersonic System and Technologies Conference, 2009 [Google Scholar]
- Lavretsky E, Wise K A. Robust and Adaptive Control with Aerospace Applications[M]. London:Springer, 2013 [CrossRef] [Google Scholar]
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