Open Access
| Issue |
MATEC Web of Conferences
Volume 65, 2016
2016 The International Conference on Nanomaterial, Semiconductor and Composite Materials (ICNSCM 2016)
|
|
|---|---|---|
| Article Number | 01004 | |
| Number of page(s) | 7 | |
| Section | Intelligent Materials and Intelligent Systems | |
| DOI | https://doi.org/10.1051/matecconf/20166501004 | |
| Published online | 06 July 2016 | |
- A., W. T. “Morphing Aircraft Systems : Historical Perspectives and Future Challenges,” Journal of Aircraft Vol. 50, No. 2, pp. 337-350(2013) [CrossRef] [Google Scholar]
- BéguinB., BreitsamterC., AdamsN., et al. “Aerodynamic Investigations of a Morphing Membrane Wing,” AIAA Journal Vol. 50, No. 11, pp. 2588–2599(2012) [CrossRef] [Google Scholar]
- TomohiroY., AyaS., and YoshiyasuH. “Development and Wind Tunnel Test of Variable Camber Morphing Wing,” 22nd AIAA/ASME/AHS Adaptive Structures Conference. American Institute of Aeronautics and Astronautics, National Harbor, Maryland, (2014). [Google Scholar]
- ValeJ., LeiteA., LauF., et al. “Aero-Structural Optimization and Performance Evaluation of a Morphing Wing with Variable Span and Camber,” Journal of Intelligent Material Systems and Structures Vol. 22, No. 10, July 1, pp. 1057–1073,(2011) [CrossRef] [Google Scholar]
- PecoraR., AmorosoF., and LecceL. “Effectiveness of Wing Twist Morphing in Roll Control,” Journal of Aircraft Vol. 49, No. 6, November-December, pp. 1666–1674,(2012) [Google Scholar]
- SpearmanM. L., and LangleyN. “Aerodynamic Research at NACA / NASA Langley Related to the Use of Variable-Sweep Wings,” 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Nashville, Tennessee, (2012) [Google Scholar]
- HallJ. “Investigation of Variable Wing-Sweep for Applications in Micro Air Vehicles,” Infotech@Aerospace. Arlington, Virginia, (2005) [Google Scholar]
- BaeJ.-S., SeiglerT. M., and InmanD. J. “Aerodynamic and Static Aeroelastic Characteristics of a Variable-Span Morphing Wing,” Journal of Aircraft Vol. 42, No. 2, March-April, pp. 528-534,(2005) [CrossRef] [Google Scholar]
- JunfuL., JunqiangA., ShituL., et al. “Research on Telescopic Wing Morphing Technology,” Advances in Aeronautical Science and Engineering Vol. 3, No. 1, pp. 2-5,2012 [Google Scholar]
- DongpingJ., and WenmeiZ. “Longitudinal flight dynamics of morphing aircraft with telescopic wings,” Chinese Journal of Applied Mechanics Vol. 31 No.3, pp. 468-472,(2014) [Google Scholar]
- AdamN., JohnV., LelandC., et al. “Morphing Aircaft Dynamical Model: Longitudinal Shape Changes,” AIAA Atmospheric Flight Mechanics Conference and Exhibit. American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, (2008) [Google Scholar]
- PeiranJ., KejunC., and LiH. Ballistics of Remote Rocket(In Chinese). China Changsha National University of Defense Technology Press, (1993) [Google Scholar]
- ZhenpingF., WanchunC., and ShuguangZ. Flight Dynamics of Aerial Vehicle(In Chinese). China Beijing: Beihang University Press, (2005) [Google Scholar]
- AdamN., JohnV., ThomasS., et al. “Six Degree-of-Freedom Dynamical Model of a Morphing Aircraft,” AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, Chicago, Illinois, (2009) [Google Scholar]
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