Works matching DE "WING-warping (Aerodynamics)"
Results: 362
Design, numerical simulation and experimental testing of a controlled electrical actuation system in a real aircraft morphing wing model.
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- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1047, doi. 10.1017/S0001924000011131
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Multi-parametric flutter analysis of a morphing wing trailing edge.
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- Aeronautical Journal, 2014, v. 118, n. 1207, p. 1063, doi. 10.1017/S000192400000974X
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Multi-body dynamic modelling and flight control for an asymmetric variable sweep morphing UAV.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 683, doi. 10.1017/S000192400000943X
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Aerodynamic study of aerofoil and wing in simulated rain environment via a two-way coupled Eulerian-Lagrangian approach.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 643, doi. 10.1017/S0001924000009416
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On the effectiveness of active aeroelastic structures for morphing aircraft.
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- Aeronautical Journal, 2013, v. 117, n. 1197, p. 1167, doi. 10.1017/S0001924000008769
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A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy Part 2: Controller implementation and validation.
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- Aeronautical Journal, 2012, v. 116, n. 1179, p. 451, doi. 10.1017/S0001924000006989
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A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy Part 1: Morphing system mechanisms and controller architecture design.
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- Aeronautical Journal, 2012, v. 116, n. 1179, p. 433, doi. 10.1017/S0001924000006977
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Thermal Manipulation in Multi‐Layered Anisotropic Materials via Computed Thermal Patterning.
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- Advanced Functional Materials, 2022, v. 32, n. 13, p. 1, doi. 10.1002/adfm.202109674
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Surrogate-based aerodynamic shape optimization of a sliding shear variable sweep wing over a wide Mach-number range with plasma constraint relaxation.
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- Structural & Multidisciplinary Optimization, 2023, v. 66, n. 3, p. 1, doi. 10.1007/s00158-023-03507-x
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A multidisciplinary design optimization for conceptual design of hybrid-electric aircraft.
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- Structural & Multidisciplinary Optimization, 2021, v. 64, n. 6, p. 3505, doi. 10.1007/s00158-021-03033-8
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Natural laminar flow wing optimization using a discrete adjoint approach.
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- Structural & Multidisciplinary Optimization, 2021, v. 64, n. 2, p. 541, doi. 10.1007/s00158-021-02936-w
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An MDO-based methodology for static aeroelastic scaling of wings under non-similar flow.
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- Structural & Multidisciplinary Optimization, 2021, v. 63, n. 3, p. 1045, doi. 10.1007/s00158-020-02804-z
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Design of cellular based structures in sandwiched morphing skin via topology optimization.
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- Structural & Multidisciplinary Optimization, 2018, v. 58, n. 5, p. 2085, doi. 10.1007/s00158-018-2020-5
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Multi-objective optimization for the geometry of trapezoidal corrugated morphing skins.
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- Structural & Multidisciplinary Optimization, 2017, v. 55, n. 1, p. 331, doi. 10.1007/s00158-016-1476-4
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Component allocation and supporting frame topology optimization using global search algorithm and morphing mesh.
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- Structural & Multidisciplinary Optimization, 2017, v. 55, n. 1, p. 297, doi. 10.1007/s00158-016-1468-4
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Aircraft morphing wing design by using partial topology optimization.
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- Structural & Multidisciplinary Optimization, 2013, v. 48, n. 6, p. 1109, doi. 10.1007/s00158-013-0944-3
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Two insulin receptors determine alternative wing morphs in planthoppers.
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- Nature, 2015, v. 519, n. 7544, p. 464, doi. 10.1038/nature14286
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Piezoaeroelastic system on the basis of a double aerodynamic pendulum.
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- ZAMM -- Journal of Applied Mathematics & Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 2021, v. 101, n. 1, p. 1, doi. 10.1002/zamm.202000092
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Bird-inspired reflexive morphing enables rudderless flight.
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- Science Robotics, 2024, v. 9, n. 96, p. 1, doi. 10.1126/scirobotics.ado4535
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Evaluation of Two-Hinged Wings.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 5, p. 267, doi. 10.2322/tjsass.64.267
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Jet Direction Control Using Circular Cylinder with Tangential Blowing.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 3, p. 181, doi. 10.2322/tjsass.64.181
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Measurement of Unsteady Aerodynamic Characteristics of a Heaving Wing in a Low Reynolds Number Flow.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 3, p. 147, doi. 10.2322/tjsass.64.147
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Effects of Propeller Position and Rotation Direction on the Ishii Wing at a Low Reynolds Number.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 1, p. 22, doi. 10.2322/tjsass.64.22
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Drag/Weight Reduction Using Split-Tip Winglet for TRA2012A Model.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 3, p. 69, doi. 10.2322/tjsass.63.69
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Aerodynamics of Owl-like Wing Model at Low Reynolds Numbers.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 1, p. 8, doi. 10.2322/tjsass.63.8
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Disappearance of Vortex Lift in Low-Aspect-Ratio Wings at Very-low Reynolds Numbers.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 6, p. 310, doi. 10.2322/tjsass.62.310
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一种基于相控阵天线的前向机载防撞系统.
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- Telecommunication Engineering, 2023, v. 63, n. 8, p. 1145, doi. 10.20079/j.issn.1001-893x.221115006
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智能材料与结构及其在智能飞行器中的应用.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 5, p. 867, doi. 10.16356/j.1005⁃2615.2022.05.012
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前缘尖化对飞翼布局飞行器气动隐身性能影响.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 2, p. 245, doi. 10.16356/j.1005⁃2615.2022.02.009
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变体机翼后缘多学科设计与优化.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2021, v. 53, n. 3, p. 415, doi. 10.16356/j.1005‑2615.2021.03.013
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变体辅助的无人机栖落机动模糊控制设计.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2020, v. 52, n. 6, p. 871, doi. 10.16356/j.1005⁃2615.2020.06.005
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扑旋翼飞行器气动特性分析及机翼拓扑优化设计.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2020, v. 52, n. 2, p. 280, doi. 10.16356/j.1005-2615.2020.02.014
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四旋翼倾转飞行器操纵冗余设计.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2020, v. 52, n. 2, p. 255, doi. 10.16356/j.1005-2615.2020.02.011
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Short-wavelength cutoff of the light bullet spectrum in calcium fluoride.
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- Applied Physics B: Lasers & Optics, 2021, v. 127, n. 3, p. 1, doi. 10.1007/s00340-021-07584-y
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Numerical Study on Aerodynamic and Aeroacoustic Performances of Bioinspired Wings.
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- Applied Bionics & Biomechanics, 2023, p. 1, doi. 10.1155/2023/9930841
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A LAMINAR FLOW, PROPULSIVE, JET-FLAPPED CONCEPT FOR ELECTRICALLY POWERED TRANSPORT AIRCRAFT.
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- Aviation (1648-7788), 2023, v. 27, n. 1, p. 14, doi. 10.3846/aviation.2023.18498
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Unsteady lifting-line theory and the influence of wake vorticity on aerodynamic loads.
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- Theoretical & Computational Fluid Dynamics, 2021, v. 35, n. 5, p. 609, doi. 10.1007/s00162-021-00578-8
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Sweep Angles Influence on the Aerodynamic Characteristics of NACA 2412 Wing with Supersonic Flow.
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- Mathematical Modelling of Engineering Problems, 2022, v. 9, n. 3, p. 757, doi. 10.18280/mmep.090323
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Optimization Efficiency of the Aircraft Wing of Cessna 172 Skyhawk by Absorbent Adverse Pressure Using Tangential Suction Slot Without Vacuum Device.
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- Mathematical Modelling of Engineering Problems, 2022, v. 9, n. 3, p. 731, doi. 10.18280/mmep.090320
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Comprehensive effects of aerodynamic performance and dynamic strength of aircraft wings after bird strike in numerical simulation.
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- Mechanics of Advanced Materials & Structures, 2024, v. 31, n. 26, p. 8564, doi. 10.1080/15376494.2024.2343039
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Aerostructural evaluation of bioinspired chordwise flexible flapping wing.
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- Mechanics of Advanced Materials & Structures, 2024, v. 31, n. 10, p. 2184, doi. 10.1080/15376494.2022.2153187
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Numerical Studies of Features of Wing Flow in the Buffeting Mode.
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- Technical Physics Letters, 2020, v. 46, n. 7, p. 633, doi. 10.1134/S1063785020070147
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PERFORMANCE ANALYSIS OF AIRCRAFT MORPHED WING WITH NACA0021 AIRFOIL.
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- Journal of the Balkan Tribological Association, 2020, v. 26, n. 2, p. 421
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Computational evaluation of flight performance of flapping-wing nano air vehicles using hierarchical coupling of nonlinear dynamic and fluid-structure interaction analyses.
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- Engineering Applications of Computational Fluid Mechanics, 2023, v. 17, n. 1, p. 1, doi. 10.1080/19942060.2023.2271053
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Morphing Wing Based on Trigonal Bipyramidal Tensegrity Structure and Parallel Mechanism.
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- Machines, 2022, v. 10, n. 10, p. 930, doi. 10.3390/machines10100930
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Investigation on the effect of leading edge tubercles of sweptback wing at low reynolds number.
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- Mechanics & Industry, 2020, v. 21, n. 6, p. 1, doi. 10.1051/meca/2020095
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A Metal Ion and Thermal-Responsive Bilayer Hydrogel Actuator Achieved by the Asymmetric Osmotic Flow of Water between Two Layers under Stimuli.
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- Polymers (20734360), 2022, v. 14, n. 19, p. 4019, doi. 10.3390/polym14194019
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Advanced Materials in 3D/4D Printing Technology.
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- Polymers (20734360), 2022, v. 14, n. 16, p. 3255, doi. 10.3390/polym14163255
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Influences of flapping modes and wing kinematics on aerodynamic performance of insect hovering flight.
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- Journal of Mechanical Science & Technology, 2020, v. 34, n. 4, p. 1603, doi. 10.1007/s12206-020-0322-1
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Numerical investigation on thrust production and unsteady mechanisms of three-dimensional oscillating wing.
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- Journal of Mechanical Science & Technology, 2019, v. 33, n. 12, p. 5889, doi. 10.1007/s12206-019-1134-z
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