Trailing-edge dynamics of a morphing NACA0012 aileron at high Reynolds number by high-speed PIV
Tài liệu tham khảo
Barbarino, 2009, A novel SMA-based concept for airfoil structural morphing, Journal of Materials Engineering and Performance, 18, 696, 10.1007/s11665-009-9356-3
Berkooz, 1993, The proper orthogonal decomposition in the analysis of turbulent flows, Annual Review of Fluid Mechanics, 25, 539, 10.1146/annurev.fl.25.010193.002543
Bilgen, 2013, Low Reynolds number behavior of a solid-state piezocomposite variable-camber wing, AIAA Journal, 1515, 8
Chen, 2008, High resolution PIV measurements around a model turbine blade trailing edge film-cooling breakout, Experiments in Fluids, 44, 199, 10.1007/s00348-007-0391-2
Chinaud, M., Boussaid, A., Rouchon, J., Duhayon, E., Deri, E., Harribey, D., Braza, M., 2012. Thermo-mechanical coupling in Nitinol. Application to an electro-morphing plate. In: XXth International Conference on Electrical Machines (ICEM). IEEE, pp. 2580–2584.
Chinaud, 2013, Hybrid electroactive wings morphing for aeronautic applications, Solid State Phenomena, 198, 200, 10.4028/www.scientific.net/SSP.198.200
Deri, 2014, Investigation of the three-dimensional turbulent near-wake structure past a flat plate by tomographic PIV at high Reynolds number, Journal of Fluids and Structures, 47, 21, 10.1016/j.jfluidstructs.2012.11.005
1995, vol. 30
Hall, S.R., Prechtl, E.F., 1999. Preliminary testing of a Mach-scaled active rotor blade with a trailing-edge servo flap. In: 1999 Symposium on Smart Structures and Materials. International Society for Optics and Photonics, pp. 14–21.
Hall, S.R., Tzianetopoulou, T., Straub, F.K., Ngo, H.T., 2000. Design and testing of a double X-frame piezoelectric actuator. In: SPIE׳s 7th Annual International Symposium on Smart Structures and Materials. International Society for Optics and Photonics, pp. 26–37.
Hee, K.H., 2012. Designing Morphing Airfoils for Improving the Aerodynamic Characteristics.
Ikeda, 1990
Jänker, P., Claeyssen, F., Grohmann, B., Christmann, M., Lorkowski, T., Leletty, R., Sosniki, O., Pages, A., 2006a. New actuators for aircraft and space applications. In: 10th International Conference on New Actuator.
Jänker, P., Hermle, F., Friedl, S., Lentner, K., Enenkl, B., Müller, C., 2006. Advanced piezoelectric servo flap system for rotor active control. In: 32nd European Rotorcraft Forum. Maastricht, The Netherlands.
Kostas, 2005, A comparison between snapshot pod analysis of piv velocity and vorticity data, Experiments in Fluids, 38, 146, 10.1007/s00348-004-0873-4
Le Letty, R., Lhermet, N., Patient, G., Claeyssen, F., Lang, M., 2002. Valves Based on Amplified Piezoelectric Actuators. online (retrieved 20.06.11). URL: http://www.cedrat.com/fileadmin/user-upload/cedrat-groupe/Publications/Publications/2002/06/Actuator2002-A4-6-VALVES-BASED-ON-AMPLIFIED-PIEZOELECTRIC-ACTUATORS.pdf.
Lumley, J.L., 1967. The structure of inhomogeneous turbulent flows. In: Atmospheric Turbulence and Radio Wave Propagation, pp. 166–178.
Mangeot, C., Andersen, B., Hilditch, R., 2009. New actuators for aerospace. In: Conference on Piezoelectric Actuation at the Institute of Mechanical Engineers (IMechE), vol. 22, London.
Manzo, J.E., 2006. Analysis and Design of a Hyper-elliptical Cambered Span Morphing Aircraft Wing (Ph.D. thesis). Cornell University.
McGowan, A.-M.R., Wilkie, W.K., Moses, R.W., Lake, R.C., Florance, J.P., Wieseman, C.D., Reaves, M.C., Taleghani, B.K., Mirick, P.H., Wilbur, M.L., 1998. Aeroservoelastic and structural dynamics research on smart structures conducted at NASA langley research center. In: 5th SPIE International Symposium on Smart Structures and Materials, San Diego, CA.
Namgoong, 2007, Aerodynamic optimization of a morphing airfoil using energy as an objective, AIAA Journal, 45, 2113, 10.2514/1.24355
Narcis Ursache, Tomas Melin, Askin Isikveren, Mike Friswell, 2007. Morphing winglets for aircraft multi-phase improvement. In: 7th AIAA ATIO Conference, 2nd CEIAT International Conference on Innovation and Integration in Aerospace Sciences, 17th LTA Systems Tech Conference; followed by 2nd TEOS Forum. Aviation Technology, Integration, and Operations (ATIO) Conferences. American Institute of Aeronautics and Astronautics, September 2007. URL: http://dx.doi.org/10.2514/6.2007-7813.
Perrin, R., 2005. Analyse physique et modélisation d’écoulements incompressibles instationnaires turbulents autour d’un cylindre circulaire à grand nombre de Reynolds (Ph.D. thesis).
Prechtl, 1999, Design of a high efficiency, large stroke, electromechanical actuator, Smart Materials and Structures, 8, 13, 10.1088/0964-1726/8/1/002
Rouchon, J.-F., Harribey, D., Derri, E., Braza, M., 2011. Activation d׳une voilure déformable par des câbles d׳AMF répartis en surface. 20ème Congrès Français de Mécanique, 28 août/2 September 2011-25044 Besançon, France (FR).
Samimy, 1991, Motion of particles with inertia in a compressible free shear layer, Physics of Fluids A: Fluid Dynamics (1989–1993), 3, 1915, 10.1063/1.857921
Straub, F.K., Kennedy, D.K., Stemple, A.D., Anand, V., Birchette, T.S., 2004. Development and Whirl Tower test of the SMART Active Flap Rotor. San Diego, CA, USA, March.