Structural and Aeroelastic Design of a Joined-Wing UAV
Publication: Journal of Aerospace Engineering
Volume 27, Issue 1
Abstract
The Italian Aerospace Research Center (CIRA) is currently designing an unmanned aerial research system that is lightweight and has high-structural flexibility, code named the High Altitude Performance Demonstrator (HAPD).The project is framed within the Italian Aerospace Research Program, under the Unmanned Aerial Vehicle (UAV) Chapter. This unmanned aerial system is mainly aimed at developing and validating advanced modeling methodologies for flexible aircrafts. A compendium of the system is provided in this paper, together with a deeper discussion of how CIRA developed the structural and aeroelastic design of HAPD. Some experimental tests performed to validate the main concepts are also presented. The vehicle has an unconventional joined-wing configuration that mitigates undesired extreme flexibility, but that results in a more complicated design. First, aeroelasticity has been taken into account from the preliminary stages of design because flexibility significantly affects aircraft behavior. Second, the HAPD structure is redundant with regard to constraints (because of its joined wing), thus making the internal forces dependent on the stiffness distribution. For these reasons, the availability of an integrated methodology that can support the structural design is mandatory. The output of such a methodology consists of primary structure stiffness distributions (fuselage, wings, and vertical tail), compatibly with the absence of any aeroelastic instability, and structural failure under operative loads.
Get full access to this article
View all available purchase options and get full access to this article.
Acknowledgments
This work was performed within a research project aimed at the preliminary design of a HAPD funded by the Italian Ministry of Instruction, University and Research through the Italian Aerospace Research Program (PRORA) in development at CIRA, the Italian Aerospace Research Center.
The writers thank Mr. Biagio Imperatore, HAPD Project Manager, for his hard work and the passion he infused to all the people involved in the project.
References
Albano, E., and Rodden, W. P. (1969). “A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.” AIAA J., 7(2), 279–285.
Bindolino, G., Ghiringhelli, G., Ricci, S., and Terraneo, M. (2010). “Multilevel structural optimization for preliminary wing-box weight estimation.” J. Aircr., 47(2), 475–489.
Breitbach, E. J. (1977). “Effect of structural nonlinearities on aircraft vibration and flutter.” Proc., 45th Structures and Materials Panel Meeting, Advisory Group for Aerospace Research and Development (AGARD), Neuilly sur Seine, France, 1–18.
Breitbach, E. J. (1980). “Flutter analysis of an airplane with multiple structural nonlinearities in the control system.” Technical Paper 1620, National Aeronautics and Space Administration (NASA) Langley Research Center, Hampton, VA, 1–36.
Cardani, C., and Mantegazza, P. (1978). “Continuation and direct solution of the flutter equation.” Comput. Structures, 8, 185–192.
Colozza, A., and Dolce, J. L. (2005). “High-altitude, long-endurance airships for coastal surveillance.” NASA Technical Memorandum, TM 2005-213427, National Aeronautics and Space Administration (NASA) Glenn Research Center, Cleveland, OH.
Dal Canto, D., Divoux, N., Frediani, A., Ghiringhelli, G. L., and Terraneo, M. (2009). “Preliminary design against flutter of a prandtlplane lifting system.” Proc., 20th National Congress for the Italian Association of Aeronautics and Astronautics (AIDAA), Associazione Italiana di Aeronautica e Astronautica (AIDAA), Rome, 1–20.
Di Palma, L., Paletta, N., and Pecora, M. (2009). “Aeroelastic design of a joined wing UAV.” Proc., SAE 2009 AeroTech Congress & Exhibition, SAE International, Troy, MI.
European Aviation Safety Agency (EASA). (2009). Certification specifications for very light aircraft CS-VLA, Amendment 1, EASA Executive Directorate, Brussels, Belgium.
Frediani, A. (2005). “The Prandtl wing.” Lecture series on innovative configuration and advanced concepts for future civil aircraft, Von Karman Institute, Brussels, Belgium, 1–23.
Frediani, A., Rizzo, E., Bottoni, C., Scanu, J., and Iezzi, G. (2006). “The PrandtlPlane aircraft configuration.” Proc., Aeronautics Days 2006, Österreichische Forschungsförderungsgesellschaft (FFG), Vienna, Austria.
Frulla, G., Cestino, E., and Marzocca, P. (2009). “Critical behaviour of slender wing configurations.” J. Aerospace Eng., 224(G), 587–600.
Gallman, J. W., and Smith, S. C. (1993). “Optimization of joined wing aircraft.” J. Aircr., 30(6), 897–905.
Hall, D. W., and Hall, S. A. (1984). “Structural sizing of a solar powered aircraft.” NASA Contractor Rep. 172313, Lockheed Missiles and Space Company, Sunnyvale, CA.
Harder, R. L., and Desmarais, R. N. (1972). “Interpolation using surface splines.” J. Aircr., 9(2), 189–191.
Imperatore, B., and Vecchione, L. (2009). “A flexible wing unmanned aerial research system.” Proc., SAE 2009 AeroTech Congress & Exhibition, SAE International, Troy, MI.
Luber, W. G. (1995). “Flutter prediction on a combat aircraft involving backlash and actuator failures on control surfaces.” Proc., Int. Forum on Aeroelasticity and Structural Dynamics, American Institute of Aeronautics and Astronautics, Reston, VA, 291–299.
MacNeal-Schwendler Corporation. (1998). MSC/NASTRAN version 70.5 – Quick reference guide. MSC Software, Santa Ana, CA.
National Aeronautics and Space Administration (NASA) Dryden Flight Research Center. (2001). “HELIOS prototype.” Dryden History, 〈http://www.nasa.gov/centers/dryden/news/ResearchUpdate/Helios/index.html〉 (Mar. 1, 2008).
Nickol, C. L., Guynn, M. D., Kohout, L. L., and Ozoroski, T. A. (2007). “High altitude long endurance air vehicle analysis of alternatives and technology requirements development.” Proc., 45th AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, Reston, VA.
Noth, A., Siegwart, R., and Engel, W. (2007). “Design of solar powered airplane for continuous flight.” Advances in unmanned aerial vehicles, Springer, Dordrecht, Netherlands, 378–405.
Paletta, N., Belardo, M., and Di Palma, L. (2011). “Non-linear dynamic loads due to the landing impact of a joined-wing UAV.” Proc., SAE 2011 AeroTech Congress & Exhibition, SAE International, Troy, MI.
Paletta, N., Belardo, M., and Pecora, M. (2010). “Load alleviation on a joined wing UAV.” J. Aircr., 47(6), 2005–2015.
Patil, M. J. (2003). “Nonlinear aeroelastic analysis of joined-wing aircraft.” Proc., 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Patil, M. J. (2007). “Nonlinear gust response of highly flexible aircraft.” Proc., 48th AIAA/ASME/ASC/AHS/ASC Structures, Structural Dynamics, and Materials Conf., American Institute of Aeronautics and Astronautics, Reston, VA.
Patil, M. J., and Hodges, D. H. (2006). “Flight dynamics of highly flexible flying wings.” J. Aircr., 43(6), 1790–1799.
Patil, M. J., Hodges, D. H., and Cesnik, C. E. S. (2001). “Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft.” J. Aircr., 38(1), 88–94.
Raghavan, B., and Patil, M. J. (2009). “Flight dynamics of high-aspect-ratio flying wings: Effect of large trim deformation.” J. Aircr., 46(5), 1808–1812.
Romeo, G., Frulla, G., Cestino, E. (2006). “Design of a high-altitude long-endurance solar-powered unmanned air vehicle for multi-payload and operations.” J. Aerospace Eng., 221(G), 199–216.
Romeo, G., Frulla, G., Cestino, E., and Corsino, G. (2004). “HELIPLAT: Design, aerodynamic, structural analysis of long-endurance solar-powered stratospheric platform.” J. Aircr., 41(6), 1505–1520.
Shen, S. (1959). “An approximate analysis of nonlinear flutter problems.” J. Aerosp. Sci., 26(1), 25–31.
Tuzcu, I., Marzocca, P., Cestino, E., Romeo, G., and Frulla, G. (2007). “Stability and control of a high-altitude, long-endurance UAV.” J. Guid. Control Dyn., 30(3), 713–721.
Wolkovitch, J. (1986). “The joined-wing: An overview.” J. Aircr., 23(3), 161–178.
Information & Authors
Information
Published In
Copyright
© 2014 American Society of Civil Engineers.
History
Received: Dec 22, 2011
Accepted: May 3, 2012
Published online: May 12, 2012
Published in print: Jan 1, 2014
Authors
Metrics & Citations
Metrics
Citations
Download citation
If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.