Open Access
| Issue |
MATEC Web Conf.
Volume 114, 2017
2017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017)
|
|
|---|---|---|
| Article Number | 02012 | |
| Number of page(s) | 9 | |
| Section | Chapter 2: Materials | |
| DOI | https://doi.org/10.1051/matecconf/201711402012 | |
| Published online | 10 July 2017 | |
- T. Smith, K. Bowcutt, J. Selmon, et al. HIFiRE 4: A Low-Cost Aerodynamics, Stability, and Control Hypersonic Flight Experiment[C]. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. (San Francisco, California. 2011). [Google Scholar]
- L. Zhang. Rapid aerodynamic shape optimization design of aircraft based on surrogate model [D].Changsha, Hunan,P.R.China:National University of Defence Technology(2015). [Google Scholar]
- J. Hu, R.H. Wang, W.J. Wang, et al. Multidisciplinary Optimization of Transport Wing Aerodynamic/Structural Integrated Design [J]. J.Nanjing Univ.Aero.& Astro. 44, 458-463 (2012). [Google Scholar]
- X. Chen, L. Liu, Z.J. Yue. A Reduced Order Modeling for Aerothermodynamic of Hypercsonic Vehicles Based on Surrogate Method [J]. Tran.Beijing Ins.Tech. 36,340-348(2016). [Google Scholar]
- Q. Gao, J.B. Zhao, Q. Li. Study on Lateral-Directional Stability of HTV-2 Like Configuration [J]. J.Astro. 36,657-662 (2014). [Google Scholar]
- X.Y. Chu. Integrated Design Method of Cruise Missile Including Configuration, Aerodynamics and Radar Stealth [D]. Nanjing:NanjingUniversity of Aeronautics and Astronautics. (2004). [Google Scholar]
- Z.H. Liu, P.L. Huang, X. Gao, et al. Multi-frequency RCS Reduction Characteristics of Shape Stealth with MLFMA with Improved MMN [J]. Chin.J.Aero. 23, 327-333 (2010). [CrossRef] [Google Scholar]
- W. Di, L. Teng, L.Y. Lin et al. Aero-Structure-Stealth Coupled Optimization for High Aspect Ratio Wing Using Adaptive Metamodeling Method [C]. 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. (Atlanta, GA. 2014). [Google Scholar]
- J.X. Su, Y. Lu, Z.Y. Zheng et al. Fast analysis and optimal design of metasurface for wideband monostatic and multi-static radar stealth [J]. J.Appl.Phys. 120,(2016). [Google Scholar]
- X.W. Jiang, Q.J. Zhao, G.G. Zhao et al. Integrated optimization analyses of aerodynamic/stealth characteristics of helicopter rotor based on surrogate model [J]. Chin.J.Aero. 28, 737-748 (2015). [CrossRef] [Google Scholar]
- J. Hu, T. Liu, P. Zhang et al. Aerodynamics/Structure/Invisibility Integrative Design and Multidisciplinary Design Optimization of Loitering Weapon [J]. Aero Weap. 3, 9-13 (2016). [Google Scholar]
- Z.H. Jiao, F. Deng, H. Liu et al. Aerodynamic and Stealthy Optimization Design Method of Hypersonic Vehicle [J]. J.Astro. 39, 1031-1040 (2016). [Google Scholar]
- K. Brenda. A universal parametric geometry representation method –“CST” [C]. 45th AIAA Aerospace Sciences Meeting and Exhibit. (Reno, Nevada. 2007). [Google Scholar]
- K. Brenda. Universal parametric geometry representation method [J]. J.Airc. 45, 142-158 (2008). [Google Scholar]
- K. Brenda, B. John. “Fundamental” parametric geometry representations for aircraft component shapes [C]. 11th AIAA/ISSMO MAOC. (Portsmouth, Virginia. 2006). [Google Scholar]
- C. Filippos. Development of code for a physical optics radar cross section prediction and analysis application [D]. California:Naval Postgraduate School. (2004). [Google Scholar]
- Y. ZRuan. Radar Cross Section and Stealth Technology [M]. Beijing: National Defence Industry Press. (1998). [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.