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Passive morphing of flying wing aircraft: Z-shaped configuration
Institution:1. Universitá del Salento, Italy;2. University of Bath, United Kingdom;1. DLR – German Aerospace Center, Institute of Composite Structures and Adaptive Systems Lilienthalplatz 7, D-38108 Braunschweig, Germany;2. Technische Universität Braunschweig, Insitute of Adaptronics and Function Integration, Langer Kamp 6, D-38106 Braunschweig, Germany;1. University of Southampton, Southampton, SO17 1BJ, UK;2. Swansea University, Singleton Park, Swansea, SA2 8PP, UK;1. Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi''an 710038, China;2. Institute of Aerodynamic and Multidisciplinary Design Optimization, National Key Laboratory of Science and Technology on Aerodynamic Design and Research, School of Aeronautics, Northwestern Polytechnical University, Xi''an 710072, China;3. State Key Laboratory of Robotics and System, Harbin Institute of Technology, Harbin, Heilongjiang Province, China
Abstract:High Altitude, Long Endurance (HALE) aircraft can achieve sustained, uninterrupted flight time if they use solar power. Wing morphing of solar powered HALE aircraft can significantly increase solar energy absorbency. An example of the kind of morphing considered in this paper requires the wings to fold so as to orient a solar panel to be hit more directly by the sun's rays at specific times of the day. An example of the kind of morphing considered in this paper requires the wings to fold so as to orient a solar panel that increases the absorption of solar energy by decreasing the angle of incidence of the solar radiation at specific times of the day. In this paper solar powered HALE flying wing aircraft are modeled with three beams with lockable hinge connections. Such aircraft are shown to be capable of morphing passively, following the sun by means of aerodynamic forces and engine thrusts. The analysis underlying NATASHA (Nonlinear Aeroelastic Trim And Stability of HALE Aircraft), a computer program that is based on geometrically exact, fully intrinsic beam equations and a finite-state induced flow model, was extended to include the ability to simulate morphing of the aircraft into a “Z” configuration. Because of the “long endurance” feature of HALE aircraft, such morphing needs to be done without relying on actuators and at as near zero energy cost as possible. The emphasis of this study is to substantially demonstrate the processes required to passively morph a flying wing into a Z-shaped configuration and back again.
Keywords:Passive morphing  Solar powered flying wing aircraft  Energy efficient flying wing  HALE aircraft  Nonlinear aeroelasticity  NATASHA
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