Open Access
Issue |
MATEC Web of Conferences
Volume 25, 2015
2015 International Conference on Energy, Materials and Manufacturing Engineering (EMME 2015)
|
|
---|---|---|
Article Number | 01011 | |
Number of page(s) | 7 | |
Section | Energy Engineering | |
DOI | https://doi.org/10.1051/matecconf/20152501011 | |
Published online | 06 October 2015 |
- Chen Zhan-jun, 2012. The study of synthetic jet improving the S-shaped inlet flow characteristics. China Science: Technology Science, 42(9):1054–1060. [Google Scholar]
- J Seddon, & E L Goldsmith. 1999. Intake Aerodynamics London: Blackwell Science. [Google Scholar]
- Zhu Yu, Luo Chang-tian, & Wang Xiao, 2005. Ultra-compact inlet airflow control technology. Aeroplane Design. (4):1–6.1 [Google Scholar]
- L.G. Hunter, & J. E. Hawkins. 1981. F-16 Variable-Geometry Inlet Design and Performance. AIAA 81–1394. [Google Scholar]
- L. E. Surber, & Lt. C. P. 1983. Robinson. Survey of Inlet Development for Supersonic Tactical Aircraft. AIAA 83–1164, [Google Scholar]
- V. Lyman, & J. P. Hancock. 1986. Correlation of Theory and Experiment for Propfan Inlets. AIAA 1986–1628, [Google Scholar]
- J. J. Korte, D. J. Singh, A. Kumar, & A. H. Auslender. 1994. Numerical Study of the Performance of Swept, Curved Compression Surface Scramjet Inlets. Journal of Propulsion and Power. 10(6). [CrossRef] [Google Scholar]
- John Fleming, & Jason Anderson. 2005. Sensing and Active Flow Control for Advanced BWB Propulsion-Airframe Integration Concepts, NASA/CR-213919. [Google Scholar]
- J. M. Abbott, & J. W. Slater. 2001. Computational Study of the Aerodynamic Performance of Three-Dimensional Subsonic Inlets. AIAA 2001–3886. [Google Scholar]
- B. L. Berrier, & B. G. Allan. 2004. Experimental and Computational Evaluation of Flush Mounted, S-Duct In-lets[R]. AIAA 2004–764. [Google Scholar]
- A. M. Kirk, A. Kumar, & J. I. Gargoloff. 2007. Numerical and Experimental Investigation of a Serpentine Inlet Duct. AIAA 2007–842. [Google Scholar]
- O. Basoglu, L. Yalcin, & A. E. Yilmaz. 2008. Computational Study on the Design Parameters of S-Type Sub-sonic Inlets. AIAA 2008–73. [Google Scholar]
- A. P. Plas, M. A. Sargeant, V. Madani, D. Crichton, E. M. Greitzer, T. P. Hynes, & C.A. Hall. 2000. Performance of a Boundary Layer Ingesting Propulsion System. AIAA 2007–450, [Google Scholar]
- Liu Zhen-xia, Guo Dong-ming, Zhang Li-fen, & Wu Dingyi. 2006. Numerical Simulation of S-shaped inlet. Paper of Aerospace Dynamic. (06) [Google Scholar]
- Zhu Yu, & Wang Xiao. 2004. Numerical Simulation of short S-shaped inlet. Aerospace Design. (04) [Google Scholar]
- Hamstra J W, Miller D N, & Truax P P, et al. 2000. Active inlet flow control technology demonstration. Aeronaut, 104(1040): 473–479 [Google Scholar]
- Zhang Yong-jun, & Feng Guo-tai. The influence of imported boundary of planar curved blade diffuser on the performance of Cascade Flow. Paper of Aerospace Dy-namic, 006, 21(2): 254–260. [Google Scholar]
- He Peng, & Dong jin-zhong, 2015. Effects of synthetic jet layout on S-shaped inlet separation control, Paper of Aerospace Dynamic, Vol. 30 No.2 Feb. [Google Scholar]
- Chen Jian-hua, 2009. Study of boundary layer suction inlet with active flow control, Harbin Industry University. [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.